Add to ORKGThrust-minus-drag forces and pressure distributions of closely spaced twin-jet afterbodies with different inboard-outboard fairing and nozzle shape
The Langley 16-foot transonic tunnel was used to determine the effects of several empennage and afte...
A three-dimensional subsonic aerodynamic panel code (VSAERO) was used to predict the effects of uppe...
A wind-tunnel investigation has been made to determine the effects of nozzle interfairing modificati...
Twin-jet afterbody models were investigated by using two balances to measure the thrust-minus-total ...
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 separately the thrust m...
Twin-jet afterbody models were investigated by using two balances to measure separately the thrust m...
Jet velocity and axial location of nozzle exit on performance of twin-jet afterbody mode
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...
A parametric study was conducted in the Langley 16-Foot Transonic Tunnel on an isolated nonaxisymmet...
The investigation was conducted at Mach numbers from 0.60 to 1.40 and jet total-pressure ratios from...
To understand / evaluate behaviour of these complex jets freestream interactions, experiments were c...
A wind-tunnel investigation to determine the effects of both single and twin jets on base drag of a ...
A parametric investigation has been conducted to determine the jet effects on the boattail drag of n...
The Langley 16-foot transonic tunnel was used to determine the effects of several empennage and afte...
A three-dimensional subsonic aerodynamic panel code (VSAERO) was used to predict the effects of uppe...
A wind-tunnel investigation has been made to determine the effects of nozzle interfairing modificati...
Twin-jet afterbody models were investigated by using two balances to measure the thrust-minus-total ...
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 separately the thrust m...
Twin-jet afterbody models were investigated by using two balances to measure separately the thrust m...
Jet velocity and axial location of nozzle exit on performance of twin-jet afterbody mode
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...
A parametric study was conducted in the Langley 16-Foot Transonic Tunnel on an isolated nonaxisymmet...
The investigation was conducted at Mach numbers from 0.60 to 1.40 and jet total-pressure ratios from...
To understand / evaluate behaviour of these complex jets freestream interactions, experiments were c...
A wind-tunnel investigation to determine the effects of both single and twin jets on base drag of a ...
A parametric investigation has been conducted to determine the jet effects on the boattail drag of n...
The Langley 16-foot transonic tunnel was used to determine the effects of several empennage and afte...
A three-dimensional subsonic aerodynamic panel code (VSAERO) was used to predict the effects of uppe...
A wind-tunnel investigation has been made to determine the effects of nozzle interfairing modificati...