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and ai is often exaggerated things and ai in its infancy states and not 100% accurateHaven't I explained above that J-36 is flying wing in "broader sense"? why failed to grasp.
No, the J-36 does not have a conventional nose in the way you might think of the rounded or conical nose on a fighter jet with a distinct fuselage.
For your further self education, this should be objective for you as it is not coming from my mouth:
View attachment 125811
and
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and
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Apology I have no choice other than posting answer from AI in order to crack stubbornness.
So the nonsense and crap is your own blabbering without adequate understanding.![]()
You know what is you talking about, Can i show the Pic of J-36 which has traditionally Stealth optimized nose cone lol

and ai is often exaggerated things and ai in its infancy states and not 100% accurate
Dude first research flying wings first, The TAILLESS designs are not necessarily means FLYINNG WING or BLENDED WING designs, there were lots of FLYING WING designs which had have vertical tails on them in past for example YB-35/YB-49 of US designs after WW2Actually, the World War II era American P-51 Mustang was not a flying wing design. It was a conventional fighter aircraft with a distinct fuselage, wings, and tail.
Flying wing designs, like the Northrop B-2 Spirit J-36 we were discussing, lack a traditional fuselage and have their crew, payload, and fuel housed within the wing structure. The P-51 Mustang has a clearly defined fuselage that houses the cockpit and engine, with wings extending from it.
Thats why, you need to understand the concept of "flying wing" in the first place.
Dude first research flying wings first, The TAILLESS designs are not necessarily means FLYINNG WING or BLENDED WING designs, there were lots of FLYING WING designs which had have vertical tails on them in past for example YB-35/YB-49 of US designs after WW2
FLYING WING or BLENDED WING designs can't go SUPERSONIC, J-36 is said be have a TOP SPEED of at least MACH 2.5, at this speed FLYING WING or BLENDED WING designs will be destroyed by AERODYNAMICS FORCES
FLYING WING and BLENDED WING designs only work best at SUBSONIC or low TANSSONIC flight (slightly below the speed of sound) FLYING WING and BLENDED WING designs CAN'T FACES AERODYNAMIC FORCES OF SUPERSONIC FLIGHT
I have question for you, Please answer my question sincerely and honestly, IF CAC DESIGNED WOULD ELIMATE VERTICAL TAILS AND CANARDS FROM J-20 WHAT YOU CALLED THIS MODIFIED J-20? FLYING WING OR TAILLESS DELTA WING?
and you talk crap again name one flying that can able to reach supersonic speed and flying wing or blended wing designs have much larger wing span than their lengths such as B-2 has length of just 69 feet but has a wing span of 170 feet, Does J-36 fits in this criteria? Clearly J-36 has shorter wing span then it length hence it is not come in the flying wing or blended wing categoriesYou talk nonsense again.
There isn't a fundamental physical law that outright prohibits a flying wing or blended wing design from reaching supersonic speeds. The principles of aerodynamics allow for various shapes to achieve supersonic flight given sufficient thrust and appropriate design.
The main challenge of flying wing to go supersonic is "drag", but it can be overcome.
Several techniques can be employed to minimize drag on a flying wing design:
The perfect example of flying wing which can speed SUPERSONIC is => J-36! LOL
- Increase Wingspan (High Aspect Ratio): A larger wingspan relative to the chord (high aspect ratio) helps to reduce induced drag, which is created by the wingtip vortices. By spreading the lift over a larger area, the intensity of these vortices is reduced.
- Optimize Wingtip Design: Wingtip devices like winglets or blended wingtips can effectively disrupt wingtip vortices, reducing induced drag and improving lift-to-drag ratio.
- Laminar Flow Control: Designing the wing to maintain a smooth, laminar flow of air over a larger portion of its surface can significantly reduce skin friction drag. This can be achieved through careful airfoil design and very smooth surface finishes.
- Smooth Surface Finish: Minimizing surface imperfections like rivets, seams, and rough paint can reduce skin friction drag. Flush rivets and smooth, carefully applied coatings are important.
- Aerodynamic Shaping (Planform Optimization): The overall shape of the flying wing, including the sweep angle and chord distribution, can be optimized to reduce wave drag, especially at higher speeds, and to manage pressure drag.
- Vortex Generators: In specific areas where flow separation might occur, small vortex generators can be used to re-energize the boundary layer and delay separation, thus reducing drag.
- Gap Seals: Sealing any gaps between control surfaces and the wing can prevent turbulent airflow and reduce drag.
- Leading and Trailing Edge Devices: Carefully designed leading and trailing edge flaps or other high-lift devices can be optimized to reduce drag during different phases of flight, not just takeoff and landing.
- Blended Wing Body Shaping: For blended wing body designs, the smooth integration of the wing and central body helps to reduce interference drag, which occurs where different aircraft components meet.
So the conclusion: Supersonic flight for these designs isn't impossible. It's just that it presents a unique set of complex engineering hurdles that need to be overcome, and the J-36 appears to be a modern example where those hurdles might have been successfully navigated.


You're way more stupid than i thought, I'm out of here from your nonsense and crap J-36 has a definitive wing and nose structures, if you're not blind you clearly seen them on various pics and videos lolAgain, you dont understand the concept of flying wing in the first place.
Allow me to repeat: "A flying wing is a tailless fixed-wing aircraft that has no definite fuselage, with its crew, payload, fuel, and equipment housed inside the main wing structure. "
So you see ... tailless wing only doesn't qualify yet the flying wing category, if other requirement (no definite fuselage) is not met!
and you talk crap again name one flying that can able to reach supersonic speed and flying wing or blended wing designs have much larger wing span than their lengths such as B-2 has length of just 69 feet but has a wing span of 170 feet, Does J-36 fits in this criteria? Clearly J-36 has shorter wing span then it length hence it is not come in the flying wing or blended wing categories
see yourself Mr.
B-2
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J-36
View attachment 125873
was I talking to you?Apples and oranges. Comparing J-36 with B-2 is like comparing P-47 with B-17.
still better than an old Vietnamese refugee MAGA that suck up to the white.Basically, a 'wing' is anything anyone on PDF who has no aviation experience interpret it to be. Just to suck up to China.
I'm comparing Both B-2 and J-36 because your friend @Antonius123 insist his crap that J-36 is flying wing or blended wing design which clearly not true for J-36 all sites is sayingJ-36 is diamond double delta wing designApples and oranges. Comparing J-36 with B-2 is like comparing P-47 with B-17.
As long as it has the word 'wing' in the description, the J-36 is a 'flying wing'. Basically, anything can be a 'flying wing'. I often mocked 'Chinese physics' all these yrs, and it looks like nothing changed.I'm comparing Both B-2 and J-36 because your friend @Antonius123 insist his crap that J-36 is flying wing or blended wing design which clearly not true for J-36 all sites is sayingJ-36 is diamond double delta wing design
Chinese dumb dumb, Vietnamese superior, happy? No matter the ethnicity, once you are a MAGA, the person will always go to the racial thing, It's pretty amazing.I often mocked 'Chinese physics' all these yrs, and it looks like nothing changed.
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