Pressure distribution on base and afterbody of missile configuration with and without jet flow using single and multiple nozzle
An investigation was made at free-stream Mach numbers of 1.62, 1.93, and 2.41 to determine the effec...
A wind tunnel investigation of the interference effects of axisymmetric nozzle air plumes, a solid p...
Experimental side and bade pressure distributions over a series of conical boattails without and wit...
An investigation has been conducted at Mach numbers of 0.6 to 1.27 to determine the effect of multip...
A wind-tunnel investigation to determine the effects of both single and twin jets on base drag of a ...
An investigation of the effects of jet nozzle geometry, size of base annulus, and base bleed upon th...
A wind tunnel investigation has been conducted at Mach numbers from 0.9 to 1.4 to determine the net-...
An investigation has been conducted in the Langley 16-Foot Transonic Tunnel to determine the effects...
The present investigation was made at a free-stream Mach number of 1.59 to compare the afterbody dra...
Base pressures were measured on fin-stabilized bodies of revolution with and without rocket chambers...
An investigation of the effects of jet nozzle geometry, size of base annulus, and base bleed upon th...
Jet velocity and axial location of nozzle exit on performance of twin-jet afterbody mode
Static pressure coefficient distributions on the forebody, afterbody, and nozzles of a 1/12 scale F-...
A parametric investigation has been conducted to determine the jet effects on the boattail drag of n...
The investigation was conducted at Mach numbers from 0.60 to 1.40 and jet total-pressure ratios from...
An investigation was made at free-stream Mach numbers of 1.62, 1.93, and 2.41 to determine the effec...
A wind tunnel investigation of the interference effects of axisymmetric nozzle air plumes, a solid p...
Experimental side and bade pressure distributions over a series of conical boattails without and wit...
An investigation has been conducted at Mach numbers of 0.6 to 1.27 to determine the effect of multip...
A wind-tunnel investigation to determine the effects of both single and twin jets on base drag of a ...
An investigation of the effects of jet nozzle geometry, size of base annulus, and base bleed upon th...
A wind tunnel investigation has been conducted at Mach numbers from 0.9 to 1.4 to determine the net-...
An investigation has been conducted in the Langley 16-Foot Transonic Tunnel to determine the effects...
The present investigation was made at a free-stream Mach number of 1.59 to compare the afterbody dra...
Base pressures were measured on fin-stabilized bodies of revolution with and without rocket chambers...
An investigation of the effects of jet nozzle geometry, size of base annulus, and base bleed upon th...
Jet velocity and axial location of nozzle exit on performance of twin-jet afterbody mode
Static pressure coefficient distributions on the forebody, afterbody, and nozzles of a 1/12 scale F-...
A parametric investigation has been conducted to determine the jet effects on the boattail drag of n...
The investigation was conducted at Mach numbers from 0.60 to 1.40 and jet total-pressure ratios from...
An investigation was made at free-stream Mach numbers of 1.62, 1.93, and 2.41 to determine the effec...
A wind tunnel investigation of the interference effects of axisymmetric nozzle air plumes, a solid p...
Experimental side and bade pressure distributions over a series of conical boattails without and wit...