Individual wing panel aerodynamic characteristics are provided for rectangular wings with aspect ratios of 0.25, 0.75, and 1.00 each panel at Mach numbers if 1.5 and 2.0 for angles of attack to 23 degrees. Data plots produced from reports of wind tunnel tests show normal force coefficients, and the spanwise and chordwise center of pressure locations
A wind tunnel test of an arrow-wing-body configuration consisting of flat and twisted wings, as well...
Force tests on a systematic series of wing systems over a range of angle of attack from minus forty-...
Wind tunnel tests of an arrow wing body configuration consisting of flat, twisted, and cambered twis...
A large amount of fundamental aerodynamic missile data, which were stored for a number of years at t...
The parts of an aerodynamics research project of the Bumblebee Program, called Generalized Missile s...
Available flow field data which can be used in validating theoretical procedures for computing flow ...
This report provides a brief description of those parts of an aerodynamics research project of the B...
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings o...
The Bumblebee program, was designed to provide a supersonic guided missile. The aerodynamics program...
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings o...
An experiment was conducted to determine wing-alone supersonic aerodynamic characteristics at high a...
Wind tunnel tests have been conducted on a research airplane model with an NASA supercritical wing t...
Pressure distribution at supersonic speeds on conically cambered wing with and without pylon mounted...
An investigation was made of the forces and moments on the cruciform aft-tail control surfaces of a ...
Pressure distributions in the form of differential pressure coefficients are presented for several w...
A wind tunnel test of an arrow-wing-body configuration consisting of flat and twisted wings, as well...
Force tests on a systematic series of wing systems over a range of angle of attack from minus forty-...
Wind tunnel tests of an arrow wing body configuration consisting of flat, twisted, and cambered twis...
A large amount of fundamental aerodynamic missile data, which were stored for a number of years at t...
The parts of an aerodynamics research project of the Bumblebee Program, called Generalized Missile s...
Available flow field data which can be used in validating theoretical procedures for computing flow ...
This report provides a brief description of those parts of an aerodynamics research project of the B...
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings o...
The Bumblebee program, was designed to provide a supersonic guided missile. The aerodynamics program...
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings o...
An experiment was conducted to determine wing-alone supersonic aerodynamic characteristics at high a...
Wind tunnel tests have been conducted on a research airplane model with an NASA supercritical wing t...
Pressure distribution at supersonic speeds on conically cambered wing with and without pylon mounted...
An investigation was made of the forces and moments on the cruciform aft-tail control surfaces of a ...
Pressure distributions in the form of differential pressure coefficients are presented for several w...
A wind tunnel test of an arrow-wing-body configuration consisting of flat and twisted wings, as well...
Force tests on a systematic series of wing systems over a range of angle of attack from minus forty-...
Wind tunnel tests of an arrow wing body configuration consisting of flat, twisted, and cambered twis...
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