Add to ORKGBasic pressure measurements on 0.0667-scale model of north american x-15 research aircraft at transonic speed
A 1/9 scale model of an existing executive type jet transport refitted with a supercritical wing was...
Flight-measured base pressures from sharp leading edge upper vertical fin of X-15 aircraft compared ...
Drag characteristics have been obtained for the X-15 airplane during unpowered flight. These data re...
Aerodynamic characteristics of scale model of X-15 research aircraft determined in transonic pressur...
Flow distribution in flight test and wind tunnel hypersonic flow of X-15 aircraf
Measured and calculated flow conditions on forward fuselage of X-15 plane and model at Mach numbers ...
Base pressure measurements have been made on the fuselage, 10 deg.-wedge vertical fin, and side fair...
Basic pressure measurements were made on a 0.087-scale model of a supercritical wing research airpla...
The tabulated results of surface pressure tests conducted on the wing and fuselage of an airplane mo...
Measurements of wing and fuselage pressure distributions were made at low and high subsonic Much num...
Static pressure coefficient distributions on the forebody, afterbody, and nozzles of a 1/12 scale F-...
Wind tunnel investigation of pressure fluctuations on the upper vertical tail of the x-15 when mated...
Experimental and calculated supersonic flutter characteristics of X-15 horizontal and vertical tail
Wind tunnel tests have been conducted on a research airplane model with an NASA supercritical wing t...
The longitudinal stability and control characteristics of a 1/30-scale model of the Republic XF-103 ...
A 1/9 scale model of an existing executive type jet transport refitted with a supercritical wing was...
Flight-measured base pressures from sharp leading edge upper vertical fin of X-15 aircraft compared ...
Drag characteristics have been obtained for the X-15 airplane during unpowered flight. These data re...
Aerodynamic characteristics of scale model of X-15 research aircraft determined in transonic pressur...
Flow distribution in flight test and wind tunnel hypersonic flow of X-15 aircraf
Measured and calculated flow conditions on forward fuselage of X-15 plane and model at Mach numbers ...
Base pressure measurements have been made on the fuselage, 10 deg.-wedge vertical fin, and side fair...
Basic pressure measurements were made on a 0.087-scale model of a supercritical wing research airpla...
The tabulated results of surface pressure tests conducted on the wing and fuselage of an airplane mo...
Measurements of wing and fuselage pressure distributions were made at low and high subsonic Much num...
Static pressure coefficient distributions on the forebody, afterbody, and nozzles of a 1/12 scale F-...
Wind tunnel investigation of pressure fluctuations on the upper vertical tail of the x-15 when mated...
Experimental and calculated supersonic flutter characteristics of X-15 horizontal and vertical tail
Wind tunnel tests have been conducted on a research airplane model with an NASA supercritical wing t...
The longitudinal stability and control characteristics of a 1/30-scale model of the Republic XF-103 ...
A 1/9 scale model of an existing executive type jet transport refitted with a supercritical wing was...
Flight-measured base pressures from sharp leading edge upper vertical fin of X-15 aircraft compared ...
Drag characteristics have been obtained for the X-15 airplane during unpowered flight. These data re...