Add to ORKGPressure tunnel investigation of supersonic store interference in vicinity of 22 deg swept wing fuselage configuration at mach numbers 1.61 and 2.0
Performance test data for pressure distributions over 60 deg delta wing at Mach 1.61 and 2.0
An investigation was performed in the Langley Unitary Plan wind tunnel to determine the aerodynamic ...
An investigation has been conducted in the Langley Unitary Plan Wind Tunnel to measure the drag of b...
Origin and distribution of supersonic store interference/measurement of individual forces on delta-w...
Effect of large store /nacelle/ on a swept-wing heavy bomber - lateral force and pitching moment
A supersonic wind-tunnel investigation on store interference has been conducted in the Langley 4- by...
A supersonic wind-tunnel investigation on store interference has been conducted in the Langley 4- by...
Supersonic store interference - 1, swept-wing heavy bomber with large stores - lift & drag at mach 1...
Aerodynamic forces and moments have been obtained in the Langley 9- by 12-inch blowdown tunnel on an...
Aerodynamic loads on external store adjacent to 60 deg delta wing at Mach numbers 0.75 to 1.9
Aerodynamic loads on high-speed aircraft external store adjacent to an unswept wing at mach 0.75 to ...
Tests were conducted in the Aerodynamic Wind Tunnel (4T) to evaluate the validity of weapon aerodyna...
A compilation is made in tabular form of all the pressures measured on a thin high-aspect-ratio wing...
Wind tunnel determination of supersonic flow properties in vicinity swept, delta, and trapezoidal wi...
Forces and moments of store-pylon combination mounting on swept wing-fuselage configuration in super...
Performance test data for pressure distributions over 60 deg delta wing at Mach 1.61 and 2.0
An investigation was performed in the Langley Unitary Plan wind tunnel to determine the aerodynamic ...
An investigation has been conducted in the Langley Unitary Plan Wind Tunnel to measure the drag of b...
Origin and distribution of supersonic store interference/measurement of individual forces on delta-w...
Effect of large store /nacelle/ on a swept-wing heavy bomber - lateral force and pitching moment
A supersonic wind-tunnel investigation on store interference has been conducted in the Langley 4- by...
A supersonic wind-tunnel investigation on store interference has been conducted in the Langley 4- by...
Supersonic store interference - 1, swept-wing heavy bomber with large stores - lift & drag at mach 1...
Aerodynamic forces and moments have been obtained in the Langley 9- by 12-inch blowdown tunnel on an...
Aerodynamic loads on external store adjacent to 60 deg delta wing at Mach numbers 0.75 to 1.9
Aerodynamic loads on high-speed aircraft external store adjacent to an unswept wing at mach 0.75 to ...
Tests were conducted in the Aerodynamic Wind Tunnel (4T) to evaluate the validity of weapon aerodyna...
A compilation is made in tabular form of all the pressures measured on a thin high-aspect-ratio wing...
Wind tunnel determination of supersonic flow properties in vicinity swept, delta, and trapezoidal wi...
Forces and moments of store-pylon combination mounting on swept wing-fuselage configuration in super...
Performance test data for pressure distributions over 60 deg delta wing at Mach 1.61 and 2.0
An investigation was performed in the Langley Unitary Plan wind tunnel to determine the aerodynamic ...
An investigation has been conducted in the Langley Unitary Plan Wind Tunnel to measure the drag of b...