Add to ORKGJet velocity and axial location of nozzle exit on performance of twin-jet afterbody mode
An investigation was conducted in the Langley 16-foot transonic tunnel to determine the induced lift...
The Langley 16-foot transonic tunnel was used to determine the effects of several empennage and afte...
The investigation was conducted at Mach numbers from 0.60 to 1.40 and jet total-pressure ratios from...
Nozzle lateral spacing effect on drag and performance of twin jet afterbody configurations with conv...
Twin-jet afterbody models were investigated by using two balances to measure the thrust-minus-total ...
Twin-jet afterbody models were investigated by using two balances to measure separately the thrust m...
Thrust-minus-drag forces and pressure distributions of closely spaced twin-jet afterbodies with diff...
Twin-jet afterbody models were investigated by using two balances to measure separately the thrust m...
A wind-tunnel investigation to determine the effects of both single and twin jets on base drag of a ...
An investigation has been conducted in the Langley 16-Foot Transonic Tunnel to determine the effects...
An investigation has been conducted in the Langley 16-Foot Transonic Tunnel to determine the effects...
The Langley 16-foot transonic tunnel was used to determine the effects of several empennage and afte...
A parametric study was conducted in the Langley 16-Foot Transonic Tunnel on an isolated nonaxisymmet...
To understand / evaluate behaviour of these complex jets freestream interactions, experiments were c...
Pressure distribution on base and afterbody of missile configuration with and without jet flow using...
An investigation was conducted in the Langley 16-foot transonic tunnel to determine the induced lift...
The Langley 16-foot transonic tunnel was used to determine the effects of several empennage and afte...
The investigation was conducted at Mach numbers from 0.60 to 1.40 and jet total-pressure ratios from...
Nozzle lateral spacing effect on drag and performance of twin jet afterbody configurations with conv...
Twin-jet afterbody models were investigated by using two balances to measure the thrust-minus-total ...
Twin-jet afterbody models were investigated by using two balances to measure separately the thrust m...
Thrust-minus-drag forces and pressure distributions of closely spaced twin-jet afterbodies with diff...
Twin-jet afterbody models were investigated by using two balances to measure separately the thrust m...
A wind-tunnel investigation to determine the effects of both single and twin jets on base drag of a ...
An investigation has been conducted in the Langley 16-Foot Transonic Tunnel to determine the effects...
An investigation has been conducted in the Langley 16-Foot Transonic Tunnel to determine the effects...
The Langley 16-foot transonic tunnel was used to determine the effects of several empennage and afte...
A parametric study was conducted in the Langley 16-Foot Transonic Tunnel on an isolated nonaxisymmet...
To understand / evaluate behaviour of these complex jets freestream interactions, experiments were c...
Pressure distribution on base and afterbody of missile configuration with and without jet flow using...
An investigation was conducted in the Langley 16-foot transonic tunnel to determine the induced lift...
The Langley 16-foot transonic tunnel was used to determine the effects of several empennage and afte...
The investigation was conducted at Mach numbers from 0.60 to 1.40 and jet total-pressure ratios from...