Add to ORKGSupersonic store interference - 1, swept-wing heavy bomber with large stores - lift & drag at mach 1.6
A method is developed for theoretically predicting the loading on pylon-mounted stores in supersonic...
The results presented in this paper indicate that the effects of stores on wing load distribution at...
Effects of wing vertical location on stability and control of canard aircraft at supersonic speed
Effect of large store /nacelle/ on a swept-wing heavy bomber - lateral force and pitching moment
Origin and distribution of supersonic store interference/measurement of individual forces on delta-w...
Pressure tunnel investigation of supersonic store interference in vicinity of 22 deg swept wing fuse...
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...
Aerodynamic forces and moments have been obtained in the Langley 9- by 12-inch blowdown tunnel on an...
An investigation has been conducted at the Langley 4- by 4-foot supersonic pressure tunnel at a Mach...
Forces and moments of store-pylon combination mounting on swept wing-fuselage configuration in super...
Aerodynamic loads on high-speed aircraft external store adjacent to an unswept wing at mach 0.75 to ...
Experimental investigations of single and twin stores representative of advanced, elliptical cross s...
An investigation has been conducted in the Langley Unitary Plan Wind Tunnel to measure the drag of b...
An investigation was made to assess the effect of wing-mounted nacelles on a supercritical wing conf...
A method is developed for theoretically predicting the loading on pylon-mounted stores in supersonic...
The results presented in this paper indicate that the effects of stores on wing load distribution at...
Effects of wing vertical location on stability and control of canard aircraft at supersonic speed
Effect of large store /nacelle/ on a swept-wing heavy bomber - lateral force and pitching moment
Origin and distribution of supersonic store interference/measurement of individual forces on delta-w...
Pressure tunnel investigation of supersonic store interference in vicinity of 22 deg swept wing fuse...
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...
Aerodynamic forces and moments have been obtained in the Langley 9- by 12-inch blowdown tunnel on an...
An investigation has been conducted at the Langley 4- by 4-foot supersonic pressure tunnel at a Mach...
Forces and moments of store-pylon combination mounting on swept wing-fuselage configuration in super...
Aerodynamic loads on high-speed aircraft external store adjacent to an unswept wing at mach 0.75 to ...
Experimental investigations of single and twin stores representative of advanced, elliptical cross s...
An investigation has been conducted in the Langley Unitary Plan Wind Tunnel to measure the drag of b...
An investigation was made to assess the effect of wing-mounted nacelles on a supercritical wing conf...
A method is developed for theoretically predicting the loading on pylon-mounted stores in supersonic...
The results presented in this paper indicate that the effects of stores on wing load distribution at...
Effects of wing vertical location on stability and control of canard aircraft at supersonic speed