Add to ORKGAerodynamic characteristics of twin jet, swept wing fighter aircraft model with leading edge Kreuger flaps at subsonic speed
Effect of rearward body strakes on transonic aerodynamic characteristics of unswept-wing fighter air...
Two sting-mounted, 50.8 cm (20 in.) span, knee-blown, jet-flap models were tested in a large (2.1- b...
This investigation was made to determine the effects of 6 degree full-spoan and 3 degree partial-spa...
An investigation has been conducted at Mach numbers ranging from 0.06 to 0.94 to determine the effec...
An investigation was conducted in the Langley 8 foot transonic pressure tunnel to determine the effe...
Recent research efforts in the improvement of the maneuverability of fighter aircraft in the high-su...
An investigation was conducted to determine the aerodynamic characteristics of a large-scale subsoni...
An investigation has been conducted in a full-scale tunnel to determine the effects of variations in...
Two 0.085-scale full span wind-tunnel models of a Mach 1.60 design supercruiser configuration were t...
An investigation of the aerodynamic performance of leading-edge flaps on three clipped delta and thr...
A low-speed investigation was conducted over an angle-of-attack range from about -4 deg to 20 deg in...
A flight program was conducted on the F-104 airplane to investigate the effects of moderate deflecti...
A general research fighter model was tested in the Langley 7 by 10 foot high speed tunnel at a Mach ...
In this study, we demonstrate the design of a Krueger flap as a substitute for a conventional slat i...
A wind tunnel investigation was conducted on a generic, high-wing transport model in the Langley 14-...
Effect of rearward body strakes on transonic aerodynamic characteristics of unswept-wing fighter air...
Two sting-mounted, 50.8 cm (20 in.) span, knee-blown, jet-flap models were tested in a large (2.1- b...
This investigation was made to determine the effects of 6 degree full-spoan and 3 degree partial-spa...
An investigation has been conducted at Mach numbers ranging from 0.06 to 0.94 to determine the effec...
An investigation was conducted in the Langley 8 foot transonic pressure tunnel to determine the effe...
Recent research efforts in the improvement of the maneuverability of fighter aircraft in the high-su...
An investigation was conducted to determine the aerodynamic characteristics of a large-scale subsoni...
An investigation has been conducted in a full-scale tunnel to determine the effects of variations in...
Two 0.085-scale full span wind-tunnel models of a Mach 1.60 design supercruiser configuration were t...
An investigation of the aerodynamic performance of leading-edge flaps on three clipped delta and thr...
A low-speed investigation was conducted over an angle-of-attack range from about -4 deg to 20 deg in...
A flight program was conducted on the F-104 airplane to investigate the effects of moderate deflecti...
A general research fighter model was tested in the Langley 7 by 10 foot high speed tunnel at a Mach ...
In this study, we demonstrate the design of a Krueger flap as a substitute for a conventional slat i...
A wind tunnel investigation was conducted on a generic, high-wing transport model in the Langley 14-...
Effect of rearward body strakes on transonic aerodynamic characteristics of unswept-wing fighter air...
Two sting-mounted, 50.8 cm (20 in.) span, knee-blown, jet-flap models were tested in a large (2.1- b...
This investigation was made to determine the effects of 6 degree full-spoan and 3 degree partial-spa...