Add to ORKGEngineering methods for predicting temperatures and velocities in vicinity of vertical lift engines of jet V/STOL aircraft operating near groun
As part of a program to improve the methods for predicting the suckdown and hot gas ingestion for je...
Several methods of predicting the compressible-flow pressure loss across a baffled aircraft-engine c...
Temperature surveys were made at the combustion-chamber outlets of a British Rolls-Royce Nene II eng...
Hot gas ingestion problems for Short Take-Off, Vertical Landing (STOVL) aircraft are typically appro...
Empirically determined wind and scale effects on hot gas recirculation characteristics of jet V/STOL...
Exhaust gas ingestion characteristics and induced aerodynamics for vertical takeoff lift engine figh...
Wind tunnel model tests of hot gas ingestion and jet interference on jet V/STOL aircraf
A flow visualization study of several configurations of a jet-powered vertical takeoff and landing (...
The development of Short Takeoff Vertical Landing (STOVL) aircraft has historically been an empirica...
The results are presented for the stagnation-point heat-transfer rates used in the design process of...
Jet VTOL fighter-type model inlet-air temperature rise analysis with various exhaust pressure ratios...
Hot gas ingestion investigation of large scale jet vertical takeoff fighter type aircraf
A 9.2 percent scale short takeoff and vertical landing (STOVL) hot gas ingestion model was designed ...
NASA Ames is conducting a program to develop improved methods for predicting suckdown and hot-gas in...
Modern jet engine design imposes extremely high loadings and temperatures on hot section components....
As part of a program to improve the methods for predicting the suckdown and hot gas ingestion for je...
Several methods of predicting the compressible-flow pressure loss across a baffled aircraft-engine c...
Temperature surveys were made at the combustion-chamber outlets of a British Rolls-Royce Nene II eng...
Hot gas ingestion problems for Short Take-Off, Vertical Landing (STOVL) aircraft are typically appro...
Empirically determined wind and scale effects on hot gas recirculation characteristics of jet V/STOL...
Exhaust gas ingestion characteristics and induced aerodynamics for vertical takeoff lift engine figh...
Wind tunnel model tests of hot gas ingestion and jet interference on jet V/STOL aircraf
A flow visualization study of several configurations of a jet-powered vertical takeoff and landing (...
The development of Short Takeoff Vertical Landing (STOVL) aircraft has historically been an empirica...
The results are presented for the stagnation-point heat-transfer rates used in the design process of...
Jet VTOL fighter-type model inlet-air temperature rise analysis with various exhaust pressure ratios...
Hot gas ingestion investigation of large scale jet vertical takeoff fighter type aircraf
A 9.2 percent scale short takeoff and vertical landing (STOVL) hot gas ingestion model was designed ...
NASA Ames is conducting a program to develop improved methods for predicting suckdown and hot-gas in...
Modern jet engine design imposes extremely high loadings and temperatures on hot section components....
As part of a program to improve the methods for predicting the suckdown and hot gas ingestion for je...
Several methods of predicting the compressible-flow pressure loss across a baffled aircraft-engine c...
Temperature surveys were made at the combustion-chamber outlets of a British Rolls-Royce Nene II eng...