1-24 of 39 Books
Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel
Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel
By P. S. Barna
Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle
Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle
By Stephen W. D. Wolf
Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure
Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure
By M. Moin Hussaini
Supersonic laminar flow control research
Supersonic laminar flow control research
By Ching F. Lo
Aerodynamic design optimization via reduced Hessian SQP with solution refining
Aerodynamic design optimization via reduced Hessian SQP with solution refining
By Dan Feng
Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research
Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research
By Steven P. Schneider
Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle
Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle
By Karen A. Deere
Nozzle thrust optimization while reducing jet noise
Nozzle thrust optimization while reducing jet noise
By John M. Seiner
First NASA/Industry High Speed Research Program Nozzle Symposium
First NASA/Industry High Speed Research Program Nozzle Symposium
By First NASA/Industry High Speed Research Program Nozzle Symposium (1992 Cleveland, Ohio)
Flight motor set 360L001 (STS-26R)
Flight motor set 360L001 (STS-26R)
By Russell J. George
The noise reduction potential of dual-stream coaxial rectangular improperly expanded jet flows
The noise reduction potential of dual-stream coaxial rectangular improperly expanded jet flows
By Darshan Dosanjh
Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air
Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air
By W. I. Scallion
Dual-throat thruster thermal model
Dual-throat thruster thermal model
By R. L. Ewen
Development of three-dimensional code for the analysis of jet mixing problem
Development of three-dimensional code for the analysis of jet mixing problem
By Khaled S. Abdol-Hamid
Shear flow control of cold and heated rectangular jets by mechanical tabs
Shear flow control of cold and heated rectangular jets by mechanical tabs
By W. H. Brown
Design of an axisymmetric, contoured nozzle for the HEG
Design of an axisymmetric, contoured nozzle for the HEG
By Klaus Hannemann
Combined numerical/analytical perturbation solutions of the Navier-Stokes equations for aerodynamic ejector/mixer nozzle flows
Combined numerical/analytical perturbation solutions of the Navier-Stokes equations for aerodynamic ejector/mixer nozzle flows
By Lawrence Justin DeChant
Contoured nozzle design and evaluation for hotshot wind tunnels
Contoured nozzle design and evaluation for hotshot wind tunnels
By E. E. Edenfield
Velocity and temperature decay characteristics of inverted-profile jets
Velocity and temperature decay characteristics of inverted-profile jets
By U. Von Glahn
Advanced small rocket chambers option 3
Advanced small rocket chambers option 3
By Donald M. Jassowski
Decomposing solid micropropulsion nozzle performance issues
Decomposing solid micropropulsion nozzle performance issues
By Brian D. Reed
Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m(2) (350 psia)
Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m(2) (350 psia)
By Tamara A. Smith
Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability
Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability
By George T. Carson