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http://forums.bharat-rakshak.com/viewtopic.php?f=10&t=5557&start=1800
Relaxed stability (which requires FBW) improves performance of all aircraft, delta, canard, and aft tail configurations. With relaxed stability, drag is reduced, fuel efficiency improved, and maneuverability is improved.
The very simple and obvious reason for this is that for aerodynamic stability, the wing and control surfaces have to be arranged in a way that requires permanent trim forces, and temporary turning forces during maneuvering that oppose the lift the wing is generating. This is worst on a delta, better on a canard and best on a aft tail configuration.
This is the reason why all commercial civil airliners built currently use relaxed stability and FBW - it reduces fuel consumption and allows greater variance in center of gravity.
Relaxed stability gives the best improvement in the case of a delta wing, which is not very maneuverable and sheds speed on turning more than the others without FBW, but a delta with relaxed stability can be as good as an aft tail with relaxed stability.
The low aspect ratio of the delta will of course create more drag than a high aspect wing especially during turning, but the Mig 21, F15, and PAKFA are all aft tail aircraft with similar low aspect ratio wings.
The reason why the reverse cranked arrow wing was used in the LCA (ie. with the root sweep less than the rest of the wing rather than greater in the case of LERX wing root extensions) was to ensure controllability at high AOA.
One of the nasty characteristics of deltas is that at high AOA the flow flips suddenly from a LERX vortex generated at the wing root, to air flowing straight over the fuselage.
It is not so much a problem if wing stall, but of maintaining pitch control of the aircraft when this happens. This was a problem with the SAAB Draken and the SAAB Viggen had an LCA like reverse crank in its wing presumably to avoid this problem.
The Mirage 2000 has strakes just ahead and above the wing to try to prevent this by forcing the vortex at all times. The Kfir used small fixed canards in the same place to direct the airflow backwards to delay the flip in airflow.
Relaxed stability (which requires FBW) improves performance of all aircraft, delta, canard, and aft tail configurations. With relaxed stability, drag is reduced, fuel efficiency improved, and maneuverability is improved.
The very simple and obvious reason for this is that for aerodynamic stability, the wing and control surfaces have to be arranged in a way that requires permanent trim forces, and temporary turning forces during maneuvering that oppose the lift the wing is generating. This is worst on a delta, better on a canard and best on a aft tail configuration.
This is the reason why all commercial civil airliners built currently use relaxed stability and FBW - it reduces fuel consumption and allows greater variance in center of gravity.
Relaxed stability gives the best improvement in the case of a delta wing, which is not very maneuverable and sheds speed on turning more than the others without FBW, but a delta with relaxed stability can be as good as an aft tail with relaxed stability.
The low aspect ratio of the delta will of course create more drag than a high aspect wing especially during turning, but the Mig 21, F15, and PAKFA are all aft tail aircraft with similar low aspect ratio wings.
The reason why the reverse cranked arrow wing was used in the LCA (ie. with the root sweep less than the rest of the wing rather than greater in the case of LERX wing root extensions) was to ensure controllability at high AOA.
One of the nasty characteristics of deltas is that at high AOA the flow flips suddenly from a LERX vortex generated at the wing root, to air flowing straight over the fuselage.
It is not so much a problem if wing stall, but of maintaining pitch control of the aircraft when this happens. This was a problem with the SAAB Draken and the SAAB Viggen had an LCA like reverse crank in its wing presumably to avoid this problem.
The Mirage 2000 has strakes just ahead and above the wing to try to prevent this by forcing the vortex at all times. The Kfir used small fixed canards in the same place to direct the airflow backwards to delay the flip in airflow.
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