Add to ORKGCascade tunnel tests on slotted stator, and candidate variable geometry inlet guide vane design
Closed-form equations for the lift, drag, and pitching moment coefficients of two dimensional airfoi...
Slotted axial flow compressor rotor and slotted stator tests of slot effect on performance of highly...
Evaluation of range and distortion tolerance for high Mach number transonic fan stages - Vol.
Slot effects on performance of highly loaded compressor rotor and stator blade row
Variable geometry concepts applied to guide vanes and stators in single stage compressor
Inlet flow distortion effects on single stage variable geometry guide vanes and stator
Annular cascade investigation to provide design criteria for slotted rotor and stator bladin
An advanced-design 25-foot-diameter flightworthy proprotor was tested in the NASA-Ames Large-Scale W...
Slosh design handbook - linearized fluid theory, propellant tank design, and slosh suppressio
Documented is an aeronautical geometry conversion package which translates wave-drag geometry into t...
An analytical model for calculation of ascent steady state tile loading was developed and validated ...
The evaluation of components of an advanced propulsion system for a future supersonic cruise vehicle...
Transient starting characteristics of small scale blowdown wind tunnel test facilit
The objective of this research is to increase the analytical capability of the existing TDK/BLM comp...
Feasibility of V/STOL test section in wind tunnel by using one eighth scale model of tunne
Closed-form equations for the lift, drag, and pitching moment coefficients of two dimensional airfoi...
Slotted axial flow compressor rotor and slotted stator tests of slot effect on performance of highly...
Evaluation of range and distortion tolerance for high Mach number transonic fan stages - Vol.
Slot effects on performance of highly loaded compressor rotor and stator blade row
Variable geometry concepts applied to guide vanes and stators in single stage compressor
Inlet flow distortion effects on single stage variable geometry guide vanes and stator
Annular cascade investigation to provide design criteria for slotted rotor and stator bladin
An advanced-design 25-foot-diameter flightworthy proprotor was tested in the NASA-Ames Large-Scale W...
Slosh design handbook - linearized fluid theory, propellant tank design, and slosh suppressio
Documented is an aeronautical geometry conversion package which translates wave-drag geometry into t...
An analytical model for calculation of ascent steady state tile loading was developed and validated ...
The evaluation of components of an advanced propulsion system for a future supersonic cruise vehicle...
Transient starting characteristics of small scale blowdown wind tunnel test facilit
The objective of this research is to increase the analytical capability of the existing TDK/BLM comp...
Feasibility of V/STOL test section in wind tunnel by using one eighth scale model of tunne
Closed-form equations for the lift, drag, and pitching moment coefficients of two dimensional airfoi...
Slotted axial flow compressor rotor and slotted stator tests of slot effect on performance of highly...
Evaluation of range and distortion tolerance for high Mach number transonic fan stages - Vol.