Table of Contents

Aerodynamics Series

레이블이 German인 게시물을 표시합니다. 모든 게시물 표시
레이블이 German인 게시물을 표시합니다. 모든 게시물 표시

2020년 4월 23일 목요일

German decides replacement for Tornado ECR and IDS(?)


Previous related Articles


 German's Luftwaffe decide to buy 30 Super Hornet w/ Nuclear capability and 15 Growler as a replacement for the aged Tornado IDS and ECR (https://theaviationgeekclub.com/germany-approves-super-hornet-growler-buy-to-replace-luftwaffe-tornado-fighter-bombers/). 

 As shown in the Airbus' plan, France and German try to develop a New jet fighter for their own Air-Force, however, aged Tornado fleet probably needs more urgent replacement than the mock-up stage aircraft. Indeed, Super Hornet would be selected as a new platform of the Luftwaffe. 

 Now, Boeing, maker of Super Hornet, has new customer for its manned military jet fighter, and they could propose their upgrade options like weapon pod or conformal fuel tank. (https://jaesan-aero.blogspot.com/2018/02/weapon-pod-for-super-advanced-hornet.html)

 Interesting point is that Luftwaffe also orders more Eurofighter as a partner of the Super Hornet. Super Hornet is generally regarded as a more Air-to-Ground mission platform than the Eurofighter. Although Eurofighter tried to expand their role to AtG mission, German might not satisfy the compatibility of the Eurofighter. 

 It will be interesting that German requires Nuclear capability for the Super Hornet. And what will be other 'German Options' for the Super Hornet?






2019년 8월 2일 금요일

New-wing concept from Airbus



 RC-scaled demonstration of New-wing concept; wing-tip part is freely moved to adapt the flow condition. 

 Expected impact is lowering gust-load and better handling quality. 


2019년 6월 17일 월요일

You-Tube Channel recommendation for Aviation Area


My recent favorite New-Channel for Aviation Area : it is quick and give direct news

 -> DJ's Aviation

New fighter jet proposal for Replacement of Tornado jet...(5) - French-German New Jet Fighter


As a consequence of proposal of French-German New jet fighter

Previous related Articles

 -> Small Note for Concept of 6th Generation Fighters : And Future Aerial-Warfare

 -> French-German's proposal for replacement of Tornado jet

 -> French-German's proposal for replacement of Tornado jet (2)

 -> French-German's proposal for replacement of Tornado jet (3)

 -> French-German's proposal for replacement of Tornado jet (4)


 Now, There are some updates for this jets from Paris Air Show. Compare to its previous concept art, additional V-tails are noticeable while fore-body part including LEX, intake is heavily modified. 

 Also, two-seated concept seems to be abandoned. In overall, previous art is similar to Pak-Fa, however, now, it is more similar to F-35 or Tempest from BAE.







2019년 4월 20일 토요일

Comparison of Airliner's Wing plan-form


 Comparison of Airliner's Wing plan-form

 As my personnel interest, I figured out wing plan-form of the modern airliners. Mainly, aircraft of Airbus and Boeing are compared in few ways to find design characteristics of the wing. 

You should know that performance of the aircraft is not only determined by the plan-form also by several factors like airfoil section, structure, position-of-wing, engine performance, and drag management. I hope you to see this article as 'fun-purpose' rather than serious 'performance comparison review'. 


1) AIRBUS family


 This shows direct comparison between Airbus-families including narrow and wide-bodies. As you could see that A330 and A340 is almost identical while the new two-engine-A35K has same size as A340. 



 Now the smallest A320's wing has smallest swept angle among the Airbus', and as aircraft goes heavy, wing has more swept angle. You could see A320 and 330 has almost similar AR except change of swept angle. In normalized view, even position of the engine is similar for A320 and 330 while more swept angle of the 330's wing is compensated by frontal-position of the engine. It is interesting to see that A320 and 330. 
 Relatively newer and heavier 350 and 380 has deeper swept angle and smaller AR than previous generation because span of the wing is limited by the practical structural and space reason. Portion of the leading edge device is also become smaller in recent generation.  


2) BOEING family

 Boeing having longer history than Airbus has more various line-up in their squad; their fancy version of classics like 777X or 747-8 will be considered in the 'Airbus-vs-Boeing'. Recent 787 and 777 show how airliner have developed in limited size for better performance.  



  You should know that trend of swept angle vs weight is kept in Boeing; heavies has deeper angle than narrow bodies or lighter ones. It showed 'engineering-convergence' strikingly strong for both of the two Airliner giants. 


3) Narrow-Bodies

 Now, we go to comparison of the two companies; both companies has their own best-seller in small-airliner class, 320 and 737. Both aircraft basically similar size however, in wing plan-form, layout is little bit different. 
 320 has more glider-like wing than 737, little bit smaller chord length with smaller swept angle. Also, 320 having longer landing gear and outer position of engine could adopt larger radius of the engine. While 320 has longer root section and outer aileron part. 
 If both aircraft have same airfoil section, 320 seems better efficiency at low speed region. We already know that low-speed region, take-off, climb, descent, and landing, takes relatively large portion of the flight-profile of narrow-bodies. 



 I have added 757 for this comparison, larger narrow-bodies, which will be replaced by Boeing's future NMA called 797. Basically, blue and green line has almost same profile except AR and engine position. In order to overcome the weight increase of 757, root-chord length is extended and engine is positioned at outer position. 


4) 330 vs Boeing's

 Tendency of 320 vs 737 is kept here; Airbus has smaller swept angle and root chord length. While 330 has longer span than 767, much frontal-position of the engine. 



 Newer 787 series has wider wing-span than 767 and become similar. Still, Boeing has deeper swept angle, and wider engine position for larger engine. 



 For three airliners, 330, 767, and 787, except engine position, Boeing family has similar layout than Airbus. Advanced wing-tip shape and longer root-section are noticeable for 787; it corresponds higher lift efficiency and heavier weight. 



 For two aircraft, difference of the swept angle is smaller than other two family comparison. Also, position of the engine is similar while 777 has longer span and root-chord length for its heavier weight. You could see that engine of the 777 is very large for its era. 
 Raked wing-tip makes noticeable difference at the tip. 


5) 350 vs 787 - Newest line-up

 Most striking feature of this comparison is here. Their newest aircraft from clean sheet is very similar for wing plan-form; only difference is probably its sizing scale. Generally, 350 is larger aircraft however, even layout of control surface is similar for each other. 
 We should watch Boeing's NMA that how they designed the wing plan-form from clean sheet; NMA is similar to 350 and 787 style or not. 



6) 350 vs 777 - Between Two-flag ships


 Actually, size of the 350 is positioned between 777 and 787, so comparison for the 350 is also done for 777. As the 350 is changed from glider-style to 787 style, now you could see Airbus has deeper swept angle than the Boeing's Classic. 777 has narrower engine position than 350 although they had larger radius engine. 
 777x extend its span and give smaller swept angle than previous aircraft to overcome increased weight. It is noticeable that making smaller swept angle is not recent trend.  



 7) 380 vs 747 - Four-engine symbols 

 Giants of two airliner giants, 380 and 747, are compared; 380 is 25% larger than 747 based on MTOW. Definitely, 380 has much larger wing than 747; it has smaller swept angle, wider span, and longer chord length. 
 Even, wings are normalized, 380's wing has bigger AR. 



 Now, we move on to add new generation of the 747-8, 




 748 has new wing with wider span, wing-tip and bigger engine. Its wing-tip is similar to 777 style. However, still, 380 is much larger aircraft than 747. Comparison of style is more convenient at normalized configuration. 
 In normalized configuration, position of the engine become very similar for 748. Modified 748 now has larger AR via added raked wing-tip. 


 8) Summary

* Mostly, Airbus has smaller swept angle than Boeing's similar class (320 and 330)

 * 330 and 340 is almost same configuration

 * Heavies has deeper swept angle and longer chord than narrow-bodies for both Airbus and Boeing

 * The newest clean-sheets, 350 and 787, has very similar design; Airbus now has highly swept one

 * New generation of Boeing, 777x and 748, has extended wing-tip

 * 777x has smaller swept angle than its predecessor; becoming Airbus style (?)



2018년 9월 2일 일요일

Small Note for Concept of 6th Generation Fighters : And Future Aerial-Warfare

* Related my previous articles for 6th Gen. Fighters (Also for Hypersonic MIRV Air-to-Air Missile)
  * Related my previous articles for Stealth Tankers (USN's MQ-25 and USAF's Stealth Tanker project)
   -> Boeing's-mq-25-candidate is revealed (2018.03.08)
   -> Lockheed's-mq-25-candidate is-revealed (2018.03.26)
   -> General Atomics'-mq-25-candidate is-revealed (2018.04.02)
   -> Additional-image-is-revealed-for MQ-25 of Boeing (2018.04.07)
   -> Additional-image-is-released-for MQ-25 of Lockheed (2018.04.09)
   -> Stealth-tanker-model-from-AFRL and Lockheed (2018.06.30)
   -> Boeing's design is Now MQ-25 (2018.08.31)
   -> Boeing MQ-25 - Additional Images (2018.08.31) 




1. Background of 6th Generation fighter
1.1. Big ice age for jet fighters: Collapse of Soviet Union and War on Terror
 As described in the previous articles or numerous phenomenon in aerospace industry, after collapse of Soviet Union in 1990’s, development of a new air-warfare weapon became sluggish or even cancelled like A-12 of USN or RAH-66 of Army as shown in Fig. 1.1. This event made USN, USAF and air-borne of US army concentrate exhausted CAS missions; fancy maneuverability or acceleration/speed was no longer required for Afghanistan or Iraq. Russia, descendant of Soviet, lost their willing for new fighters because of their economic chaos; only demonstrators like MiG-1.44, Su-37, or 47 were in show-window.

 Frankly, about for 25 years after the collapse, there was no equivalent rival for F-15 with AIM-120C, and this had been proved by record; most of the Su-27 series were limited in usage of R-27. War on Terror and sub-prime mortgage consumed certain part of the defense budget, and there was no room for ‘already-the-best-area-of-USAF’; amount of production for F-22 was also reduced. USN should adopt F/A-18E/F as replacement of glory F-14 and A-6 for cost reason; Congress did not allow expensive stealth jet for ‘GBU-truck’ missions.

 F-22 and F-35 was the latest jet fighters developed by US just before end of the Cold War; F-22 pursued for countering-all-imaginable-threat while F-35 tried to make entire air-fleet as sum of F-16 and F-117 with reasonable(?) cost. This kind of approach still showed glimpse of Cold-War age idea which try to overwhelm rival Russia in every aspect. Naturally, these had been criticized by internal enemies arguing their cost. It looked reasonable that special ability for day-1 strike was no-longer represented in Pax-Americana, and all-stealth of entire air-fleet is still argued topic for constitute of high air-command. So, it is not surprising that proliferation of unmanned concept for reducing ‘human-exhaust or risk’ and cost was fancy at that time. Mission of ISR or police type patrol could be replaced by relatively simple platforms, and few of them bear fruit like MQ-1, 9 or Global Hawk.



Fig. 1.1. Two typical example of “Cancelled as Collapse of Soviet Union”, A-12 and RAH-66; Cost is not only problem for these, also ‘too-strong-or-expensive’ for War-on-Terror. They lost their primary adversary at early 90’s.


Fig. 1.2. The two latest jet fighter projects of US, F-22 and 35, were criticized for its in-effectiveness in cost for Ice-age, however is it right again for new Cold-War age?


1.2. Advent of T-50 and J-20
As the US have struggled in desert, global power of Russia was partially restored, and Chinese pursued regional power in western Pacific. Aspiration of the two countries was proved by prototype of T-50 and J-20 as shown in Fig. 1.3, challenging air-superiority of US. Two aircraft is similar or larger than F-22; clearly they pursue super-cruise, stealth, and high maneuverability performance like that of F-22. Still, exact performance of the two are in fog via unfinished development of them, however it clearly showed long-lived high teen series will face end of their prime time. If we changed our focus from ‘common between F-22 and its rivals’ to ‘differentiation’, physical size of the two fighters are noticeable. They prepare long range missions to cover their deep territory or have intention to penetrate air-space.

Penetration of air-space with long range is essential for 1st class of air-superiority fighters requiring sniping of prime assets guarded by their own escort fighters like AWACS, Tankers, and Bombers. That kinds of mission profiles were limitedly supported by Su-27 class fighters in Cold-War age with specially designed air-to-air missiles, Kh-31A/P or KS-172. Proof of the intention is clearly shown for these fighters; both fighters have deep internal weapon bays for long range missiles like new R-37M class as shown in Fig. 1.3. With combination of enhanced long range missiles and stealth performance of them, threat for US air-superiority is not only for front-line fighters also for the prime assets.

Contrary to Chinese and Russian, European did not show any noticeable movement related to development of fighters like F-22, J-20, or T-50. They have struggled much time for Eurofighter and Rafale, and satisfied a few number of F-35 during the Ice Age of jet fighters. They have concentrated development of cruise missiles and UCAV projects for Day-1 Strike missions.



Fig. 1.3. J-20 (Top) and T-50 (Middle) are result of two countries challenging air-superiority of USAF and USN. Bottom view of T-50 (Bottom) shows R-37M class long range missiles (blue) could be carried internal bay of the T-50.


1.3. Current Limit of 5th Generation fighters: Range/Loitering of Current Platform
USAF and USN are the most sensitive forces in the world for the range and payload of their platform because they always did offensive role in the air-warfare. So it is not strange that size of US jet fighters is mostly bigger than their counter part except few bizarre Soviet interceptors, Yak-128, MiG-25 and 31. As shown in the Fig. 1.4, F-22 and F-35 invest much of their internal space for fuel, however, basically, stealth performance requires limitation of external fuel tank and consume internal space as weapon bay, then, leads to short range.

Advent of enemy’s advance air-defense system including fighters (J-20, T-50, and J-31) and SAMs (S-300, 400, and 500) aggravate the situation worse as it limits ‘safe-range’ from enemy territory for aerial refueling or external fuel tank. Also it is bonus that Russia and China has very deep offensive depth via size of their land. For F-22, 1st capable super cruiser, problem is not negligible; advantage of super-cruise is unavoidably consuming a lot of fuel.



Fig. 1.4. Internal fuel tank layout or cutaway of F-22 (Top), F-35 (Middle), and T-50 (Bottom). As attachment of external fuel tank is limited by stealth, space for internal tank become more important.



2. Concepts of 6th Generation fighters
After advent of J-20 and T-50 for 10 years, whether western countries developed 5th generation fighters or not, western counter parts showed their plan for the jet fighters breaking the ice age. Fortunately, their plan is well summarized in Fig. 2.1 with uncertainties; political, technical, or budget issues always changed what they planned. Among the planned fighters, T-50 and J-20 are the initial triggers for the other jet fighters; from the plan, absolute advantage of US’ F-22 and F-35 will be challenged by Russian and Chinese at 2020, and US’ answer will be prepared at 2030.

Plan for other fighters like India, Korea, Turkey, Japan is uncertain to ‘overwhelm’ the Chinese and Russian due to lack of experience for leading air-warfare technologies. Even in the Korean case, target of the jet fighter performance is limited in 4.5th generation fighter for Block I; full performance of Block III is expected to be slightly worse than 5th generation fighters. Project of India always suffers long delay as shown in the project of Tejas. Turkish has lack of experience in full-scale jet fighters like Korean while Japanese has possibilities of conducting better fighter than others. However, willing to develop Japanese fighter is still uncertain.

Indeed, this article focuses on 6th generation fighter projects related to US, French-German, and UK having possibility to overwhelm J-20 and T-50.



Fig. 2.1. Plan/situation of jet fighter development; about 2030, picture of air-warfare will be changed.


2.1. Common Goals presented in Concepts
Few pictures of known projects, F/A-XX, F-X, FCAS, and Tempest are shown in below from Fig. 2.2 to Fig. 2.5; all of these are still in CG concept level. We could speculate some common characteristics from these eye candies. All of them targeted extremely large platform size as fighter. Although few of them has same physical size of conventional fighters for length and span, expected payload and internal volume is much bigger than current 4th and 5th generation fighters; huge delta wing with or without tails committed it. That kind of external configuration of the jets means more loitering time/range/payload is emphasized rather than conventional dog-fighting or maneuvering. Actually, that kinds of tendency for maneuver in transonic region was already in the road of decline as R-73 emerged. Advanced SRAAMs including MICA-IR, ASRAAM, IRIS-T, R-74, Python-5, and AIM-9X already overwhelmed maneuverability of human-driven jet vehicle limited by physical condition of human (http://jaesan-aero.blogspot.com/2018/05/small-note-for-short-range-air-to-air.html).



Fig. 2.2. Few concept CG related to 6th Generation fighters for F-X of USAF from Northrop (Top), Lockheed (Middle), Boeing (Bottom)



Fig. 2.3. Few concept CG related to 6th Generation fighters for F/A-XX of USN from Boeing



Fig. 2.4. Few concept CG related to 6th Generation fighters for France-German (FCAS)



Fig. 2.5. Few concept CG related to 6th Generation fighters for UK Tempest


Indeed, all of the published concepts seems to focus wide range of weapons including DEW to cover short range engagement; combination of short range missiles and DEW act like RAM and CIWS of modern destroyers. It means new generation of fighters did not act like individual vehicle also take role of modern ship having complex layer of defense and offensive payloads. In order to keep the jet flyable status with various payloads, advanced engine is also proposed by GE and Rolls Royce which uses adaptive variable cycle engine as shown in Fig. 2.6. It is not certain that other aircraft like FCAS will carry the variable cycle engine however, similar technology should be attained to FCAS as one of competitive contender. Concept of the engine is basically controlling the bypass ratio of the jet to maximize its fuel economy; saving power is directly connected to magazine of the DEW.

Not only for its self-defense, also weapon for offensive punch already start its race as shown in Fig. 2.7. Recent race for hypersonic weapon is not irrelevant to this trend because ace in the hole for the 6th generation fighter would become hypersonic missile or glider to penetrate enemy air-defense. Miniature version of ‘Kinzhal’ missile will be popular and large volume of internal bay should be prepared for that kinds missiles. Although performance of stealth, sensors, or network capabilities are not represented in fancy art or OML shape, to maximize effectiveness of payloads or hardware of the jets, numerous videos already emphasized wide range of stealth, fused-sensors, and network capabilities with UCAVs. Commercial of USAF (http://jaesan-aero.blogspot.com/2018/03/usaf-2030-commercial.html) or replacement of tornado jet fighter by Airbus as shown in Fig 2.8 and 2.9.

Conventional jet fighter will RTB when they use all of their payload however, 6th generation fighters loiters air-space to control or provide precise ISR information to friendly air-asset. It maximized not only performance of own, also of friendly forces; it represented reality that even major countries could not replace all of their jets using 6th generation fighters. Co-operating with previous generation jet fighter or UCAV essential.

Certainly Common things in Concepts
l  Large platform for payload/endurance
l  Highly Stealth
l  ISR performance with network capabilities




Fig. 2.6. Concept of variable cycle engine by GE; it is not surprise that YF-120 had proposed similar configuration.



Fig. 2.7. One of ‘Silver Bullet’ type weapon developed for F-35 or 6th generation fighters; highly stealth or hypersonic weapon will be carried inside of the jets for day-1 strike mission.



Fig. 2.8. Network capabilities with friendly asset is continuously shown in commercial of 6th generation fighters (Airbus)



Fig. 2.9. Network capabilities with friendly asset is continuously shown in commercial of 6th generation fighters (USAF 2030)


2.2. Discrimination between Concepts
Table 1 Summary table for common and different things of 6th generation fighters’ concepts



Previous paragraph described common goals and concepts of the jets however, even in the CGs, there are some differences as shown in Table 1. First of all, we selection of seat # for each concept; most of concepts choose single seat while FCAS and F/A-XX for two seat (even F/A-XX could be unmanned). FCAS emphasized endurance on the enemy air-space and ISR role, and naturally leads to additional crew. Requirement for F/A-XX might be similar if F/A-XX replace EA-18G and F/A-18E/F series. Other jets like F-X or Tempest also emphasize that way however they show no sign of additional crew behind the pilot. We could assume that USAF has enough resources to cover needs of additional crew for the fighter, however, USN or French-German’s should cover various role in limited number of sorties.

As described in the figures and descriptions, all of the 6th generation fighter jet has large planform of the wing however, in the configuration of the tails, there is some differences. While others deleted HT as pitch control, tail surface of Lockheed still remained. Actually, Northrop’s one seems like big warship than conventional fighters, so it is the most radical approach among 6th generation fighters. Also, it is the only Northrop that air-inlet is installed upper surface of the jet and deleted TVC; upper inlet and deletion of TVC shows worst performance in conventional maneuver in air combat. Approaches of F/A-XX from Boeing, FCAS and Tempest is between Lockheed and Northrop; LEVCON of FCAS, TVC of Tempest and F/A-XX compromise between conventional maneuverability and warship like concepts.

As a payload of 6th Generation fighters, DEW is the most controversial thing; degree of maturity of DEW and other RAM style weapons, SACM and MDSM, determine dependence of conventional maneuverability. As the Northrop one more depend on technological maturity of such things, their jet become warship like bigger one. 6th generation fighters of US and UK definitely showed concept of usage of DEW while French-German one is in uncertainty. UK Tempest, revealed at most recently, showed concept of carriage of UCAV inside of IWB; in US commercial, transports or bombers will be specialized for this duty. Or maybe in USN, unmanned module is installed in F/A-XX to cooperate manned version.


2.3. Advent of Stealth Tankers
Stealth tanker proposal is another issue for USAF and USN; both are planning to develop own stealth tankers. If the tactical aircraft is non-stealth, stealth tanker itself is not pursued. And also, every tanker could not be stealth because of cost. Indeed, we could speculate stealth tanker will be member of team which consists of stealth tanker + 6th generation fighter + 5th generation fighter + UCAV + swarm of drones. That kinds of package replace conventional strike package which is armada of air fleet before stealth technology was emerged. As shown in Fig. 2.10 and 11, USN and USAF currently develop stealth tanker while USN proceed further; they already receive competition of three companies, Boeing, General Atomics, and Lockheed.

Advent of stealth tanker and long range/endurance of 6th generation fighter is not irrelevant. As the threat from J-20 and Pak-Fa become invisible and their military depth of air-defense is deeper, whole components of the strike package is under the threat. Cost of 5th and 6th generation fighter is rising; they should cover longer time of campaign with limited number of jets. It means whole strike package require large amount of fuel in one sortie, however, no tactical level jet could carry massive internal fuel for that requirement. MQ-25 of USN and Stealth tanker of USAF will never refuel for their aircraft in the enemy air-space, however, their stealth performance significantly reduces the distance from enemy air-defense system where refuel is managed. So, adaptive-variable cycle engine, large platform, and stealth tanker make synergy for perfect overwhelming of enemy air-space in spatially and temporally.




Fig. 2.10. MQ-25 : USN’s new stealth tanker



Fig. 2.11. One model of USAF’s Stealth tanker is shown.


3. Conclusion and future of further
Author had written short review for 6th generation fighters with limited information; most of them could be changed as concept is matured. Actually, need for 6th generation fighter was sluggish until threat of J-20 and Pak-Fa was realized. As they challenged technological superiority of old-western world, current edge of US Aerospace technology, F-22 and F-35 expose their weakness, high cost, short range for long depth, and small-payload.

Revealed 6th generation fighters commonly emphasize large platform for flexibility/range/payload/enhanced capability of ISR with stealth performance. Another aspect of the concept is co-work with previous generation fighter, UCAV, and stealth tankers. Advertisement of previous generation fighters always emphasized simple-overwhelming of pre-previous ones, and recommend air-forces to replace all of their jets. However, as cost of jet fighter rises sky-rocketing, number of 6th generation fighter is under the pressure. So the concepts have studied more about co-operation capability with other assets of forces, and try to maximize overall effectiveness of sorties. Unlike 5th generation fighters, 6th generation fighter does not pursue winning every aspect of previous generation fighters; the new planned fighter will take the leading role of the fighting group, containing 6th and 5th generation fighters, UCAV, and even with stealth tanker.


As they limited their role in aerial warfare, it is hard to imagine the new fighter perform fancy maneuver; DEW and small munitions guard the fighter or other friendly jet like Aegis warships. Fight of aerial fleet having multi-layered weapon and vehicle become more systematic than fight in the past. Even the new weapon emerges like hypersonic MIRV air-to-air missile (https://jaesan-aero.blogspot.com/2017/04/1-high-aoa-aerodynamics-for-combat_21.html), the fleet just need absorb the new weapon as one of their spear. It is interesting to see how evolve these concepts until 2030s.