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Reverse airflow-forward-swept wing vs aft swept wing. On the forward-swept wing, ailerons remained unstalled at high angles of attack because the air over the forward swept wing tended to flow inward toward the root of the wing rather than outward toward the wing tip as on an aft-swept wing. This provided better airflow over the ailerons and prevented stalling (loss of lift) at high angles of attack.
X-29 - designed with relaxed static stability to achieve less drag, more maneuverability, increased fuel efficiency. Arrows in upper illustration indicate drag-producing opposing downward forces on rear stabilizers to achieve stability. X-29 canards share lifting loads, reducing drag.
Wing Divergence
Another problem of the wing is the critical wing divergence (e.g. the operation point at which irreversible aeroelastic effects take place, with catastrophic consequences). This difficulty would require a much heavier wing than the corresponding backward swept wing. The problem could be partially solved with the use of advanced composite materials.
aerodyn.org...
Originally posted by intelgurl
Here are some other ATS threads that make references to the forward swept wing X-29.
Also, check out the thread entitled Rockwell Saber Bat, it was a forward swept design prior to the X-29.
The Official Best Concept Planes Thread
What are advantages of Forward Swept Wings?
Questions about wing designs
Rockwell Saber Bat
X-29 - designed with relaxed static stability to achieve less drag, more maneuverability, increased fuel efficiency. Arrows in upper illustration indicate drag-producing opposing downward forces on rear stabilizers to achieve stability. X-29 canards share lifting loads, reducing drag.
The SFW/F-16 was rejected by DARPA in January 1981 in favor of the Grumman 712 (an F-5/F-20 derivative), later designated the X-29A. The decision was mainly a political one, as many thought that the test-scene at NASA was heavily dominated by General Dynamics' F-16s (AFTI, CCV, F-16XL). Another much-cited reason was that "One could only learn so much from a single airframe", though in retrospect, ongoing experiments with the F-16 seem to prove this wrong. It is interesting to note that the chosen design, the X-29A, consists for about 16% of F-16 components, including the Fly-By-Wire Flight Control System.
Originally posted by ShadowXIX
Man I love the look of planes with FSWs I consider the SU-47 one of the best looking planes ever.
The X-Planes are indeed amazing, Im not positive but I think a X-plane was using vectored thrust before the Russians aswell.
Originally posted by Canada_EH
believe your talking about the X-31.
Originally posted by waynos
Apart from the P.1127/Harrier family (which is a different kettle of fish altogether) I think the first plane to fly with TVC installed was the F-15 ACTIVE demonstrator, the X-31 followed but I'm not sure how it stands in relation to when the Russians first had such a plane flying.
Does anyone think the X-29 could have made a decent light fighter? How would those wings stand up on a service fighter?
Originally posted by carcharodon
If I remember correctly the F-15 ACTIVE used conventional 'round' vector thrust and square vector propulsion just like the one on the Raptor.
It was the testbed for the low heat emision thrust.