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supersonic wind tunnelRoute of transportation
Wedge and scoop air inlet performance and thrust minus drag comparisons at free stream in supersonic wind tunnel test
An investigation was conducted in the 8- by 6-foot supersonic wind tunnel on the external and intern...
Wind tunnel investigation of transonic and supersonic flutter of air to surface missile vertical tai...
Supersonic performance of variable two-dimensional inlets designed for engine-inlet matching
Wind tunnel test to determine swept wing fighter aircraft drag, and logitudinal and lateral stablity...
Internal flow performance of fixed 14 deg ramp inlet from zero to 20 deg angle of attack at superson...
A general discussion of the air-inlet problem is presented. Recently obtained drag and pressure-reco...
Two normal -wedge-inlet configurations (straight and sweptback splitter plates) were investigated in...
Translating spike inlet air flow regulation characteristics from transonic to supersonic speeds at z...
An experimental investigation was conducted to determine the performance characteristics an underslu...
The supersonic free-flight wind tunnel is a facility at the Ames Laboratory of the NACA in which aer...
Performance characteristics of underslung vertical wedge inlet with porous suction at Mach numbers o...
Report presenting an investigation of a swept, rectangular, supersonic scoop inlet designed to have ...
Aerodynamic characteristics of aircraft configuration having tail surfaces outboard of wing tips at ...
Wind tunnel testing of two and four engine models of delta wing aircraft for transonic drag rise inc...
Wind tunnel test to establish validity of Fourier analysis results for transonic drag rise changes d...
An investigation was conducted in the 8- by 6-foot supersonic wind tunnel on the external and intern...
Wind tunnel investigation of transonic and supersonic flutter of air to surface missile vertical tai...
Supersonic performance of variable two-dimensional inlets designed for engine-inlet matching
Wind tunnel test to determine swept wing fighter aircraft drag, and logitudinal and lateral stablity...
Internal flow performance of fixed 14 deg ramp inlet from zero to 20 deg angle of attack at superson...
A general discussion of the air-inlet problem is presented. Recently obtained drag and pressure-reco...
Two normal -wedge-inlet configurations (straight and sweptback splitter plates) were investigated in...
Translating spike inlet air flow regulation characteristics from transonic to supersonic speeds at z...
An experimental investigation was conducted to determine the performance characteristics an underslu...
The supersonic free-flight wind tunnel is a facility at the Ames Laboratory of the NACA in which aer...
Performance characteristics of underslung vertical wedge inlet with porous suction at Mach numbers o...
Report presenting an investigation of a swept, rectangular, supersonic scoop inlet designed to have ...
Aerodynamic characteristics of aircraft configuration having tail surfaces outboard of wing tips at ...
Wind tunnel testing of two and four engine models of delta wing aircraft for transonic drag rise inc...
Wind tunnel test to establish validity of Fourier analysis results for transonic drag rise changes d...
An investigation was conducted in the 8- by 6-foot supersonic wind tunnel on the external and intern...
Wind tunnel investigation of transonic and supersonic flutter of air to surface missile vertical tai...
Supersonic performance of variable two-dimensional inlets designed for engine-inlet matching
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