Add to ORKGSimulated flight tests of elastic swept-wing bomber and fighter model coupled wing tip to wing tip
Force tests on a systematic series of wing systems over a range of angle of attack from minus forty-...
Aerodynamic characteristics of aircraft configuration having tail surfaces outboard of wing tips at ...
Low speed aerodynamic characteristics of swept- wing aircraft with blowing flaps and leading-edge sl...
Wind tunnel testing of swept wing fighter aircraft model for determining drag and static longitudina...
Wind tunnel tests of swept-wing fighter aircraft with spoiler-slot-deflector lateral control system
Wind tunnel investigations of effect on static stability of modifications to swept wing fighter airc...
Wind tunnel test to determine swept wing fighter aircraft drag, and logitudinal and lateral stablity...
Free flight tunnel testing of swept wing aircraft model to determine roll effectiveness of different...
Subsonic and supersonic wind tunnel study of low aspect ratio sweptback wing tailless fighter aircra...
An investigation has been made by the NACA wing-flow method to provide information on the relative l...
Longitudinal and lateral stability and control characteristics of swept wing fighter aircraft
Low-speed free flight tunnel testing of swept wing fighter aircraft for determining effect of small ...
Wind tunnel tests haved been made at low speed to various small-scale models of swept-back, swept-fo...
Force and pressure distribution studies to high angles of attack on all-movable triangular and recta...
Wind tunnel investigation of transonic and supersonic flutter of air to surface missile vertical tai...
Force tests on a systematic series of wing systems over a range of angle of attack from minus forty-...
Aerodynamic characteristics of aircraft configuration having tail surfaces outboard of wing tips at ...
Low speed aerodynamic characteristics of swept- wing aircraft with blowing flaps and leading-edge sl...
Wind tunnel testing of swept wing fighter aircraft model for determining drag and static longitudina...
Wind tunnel tests of swept-wing fighter aircraft with spoiler-slot-deflector lateral control system
Wind tunnel investigations of effect on static stability of modifications to swept wing fighter airc...
Wind tunnel test to determine swept wing fighter aircraft drag, and logitudinal and lateral stablity...
Free flight tunnel testing of swept wing aircraft model to determine roll effectiveness of different...
Subsonic and supersonic wind tunnel study of low aspect ratio sweptback wing tailless fighter aircra...
An investigation has been made by the NACA wing-flow method to provide information on the relative l...
Longitudinal and lateral stability and control characteristics of swept wing fighter aircraft
Low-speed free flight tunnel testing of swept wing fighter aircraft for determining effect of small ...
Wind tunnel tests haved been made at low speed to various small-scale models of swept-back, swept-fo...
Force and pressure distribution studies to high angles of attack on all-movable triangular and recta...
Wind tunnel investigation of transonic and supersonic flutter of air to surface missile vertical tai...
Force tests on a systematic series of wing systems over a range of angle of attack from minus forty-...
Aerodynamic characteristics of aircraft configuration having tail surfaces outboard of wing tips at ...
Low speed aerodynamic characteristics of swept- wing aircraft with blowing flaps and leading-edge sl...