Add to ORKGThe selection procedure is described which was used to arrive at the configurations tested, and the ...
Aerodynamics research in rarefied gas dynamics, base heating, and turbulent fluctuation
Mr. Ruf of NASA/MSFC executed the CHEM computational fluid dynamics (CFD) code to provide a predicti...
A calibration was made of the acoustic and aerodynamic characteristics of a small, open-jet wind tun...
Test data is presented which allows determination of jet penetration and mixing of multiple cold air...
The National Transonic Facility (NTF) was operated to design condition of 120 million Reynolds numbe...
Static rocket thrust chamber simulator for cylindrical cold flow-type apparatus desig
A wind-tunnel investigation of the NASA SC(2)-0012 airfoil has been conducted in the Langley 0.3-Met...
Jet spreading in fluid amplifiers, thermal switching of jet flows, and nozzle thrust modulation by v...
Cold wire measurement of temperature fluctuations were made in a DERAT T'2 induction powered cryogen...
A one-dimensional distributed-parameter dynamic model of a cryogenic wind tunnel was developed which...
The National Transonic Facility (NTF) was operational in a combined checkout and test mode for about...
The flow field in and around the nozzle afterbody section of a hypersonic vehicle was computationall...
Thrust modulation techniques - cold flow tests of three variable-throat-area convergent-divergent no...
Theoretical considerations indicate that cooling the wind-tunnel test gas to cryogenic temperatures ...
The selection procedure is described which was used to arrive at the configurations tested, and the ...
Aerodynamics research in rarefied gas dynamics, base heating, and turbulent fluctuation
Mr. Ruf of NASA/MSFC executed the CHEM computational fluid dynamics (CFD) code to provide a predicti...
A calibration was made of the acoustic and aerodynamic characteristics of a small, open-jet wind tun...
Test data is presented which allows determination of jet penetration and mixing of multiple cold air...
The National Transonic Facility (NTF) was operated to design condition of 120 million Reynolds numbe...
Static rocket thrust chamber simulator for cylindrical cold flow-type apparatus desig
A wind-tunnel investigation of the NASA SC(2)-0012 airfoil has been conducted in the Langley 0.3-Met...
Jet spreading in fluid amplifiers, thermal switching of jet flows, and nozzle thrust modulation by v...
Cold wire measurement of temperature fluctuations were made in a DERAT T'2 induction powered cryogen...
A one-dimensional distributed-parameter dynamic model of a cryogenic wind tunnel was developed which...
The National Transonic Facility (NTF) was operational in a combined checkout and test mode for about...
The flow field in and around the nozzle afterbody section of a hypersonic vehicle was computationall...
Thrust modulation techniques - cold flow tests of three variable-throat-area convergent-divergent no...
Theoretical considerations indicate that cooling the wind-tunnel test gas to cryogenic temperatures ...
The selection procedure is described which was used to arrive at the configurations tested, and the ...
Aerodynamics research in rarefied gas dynamics, base heating, and turbulent fluctuation
Mr. Ruf of NASA/MSFC executed the CHEM computational fluid dynamics (CFD) code to provide a predicti...