1-24 of 35 Books
Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept
Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept
By David E. Hahne
Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements
Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements
By W. Lance Richards
Three-dimensional Navier-Stokes simulations with two-equation turbulence models of intersecting shock-waves/turbulent boundary layer at Mach 8.3
Three-dimensional Navier-Stokes simulations with two-equation turbulence models of intersecting shock-waves/turbulent boundary layer at Mach 8.3
By J. E. Bardina
Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel
Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel
By Glen P. Doggett
Shock-tunnel combustor testing for hypersonic vehicles
Shock-tunnel combustor testing for hypersonic vehicles
By Mark Loomis
Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6
Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6
By Floyd J. Wilcox
Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment
Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment
By Leslie Gong
Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program
Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program
By Alexander S. Roudakov
Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0
Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0
By Ramadas K. Prabhu
Hypersonic flows as related to the national aerospace plane
Hypersonic flows as related to the national aerospace plane
By Marvin Kussoy
A first scramjet study
A first scramjet study
By George Emmanuel
Physics of interplanetary dust collection with aerogel
Physics of interplanetary dust collection with aerogel
By William W. Anderson
Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code
Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code
By Kamlesh Kapoor
Mach 10 experimental database of a three-dimensional scramjet inlet flow field
Mach 10 experimental database of a three-dimensional scramjet inlet flow field
By Scott D. Holland
Turbulence modeling
Turbulence modeling
By Jorge E. Bardina
Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system
Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system
By J. R. DeBonis
Transition at hypersonic speeds
Transition at hypersonic speeds
By Mark Vladimir Morkovin
The NASA Hyper-X Program
The NASA Hyper-X Program
By D. Freeman
Application of CFD to the analysis and design of high-speed inlets
Application of CFD to the analysis and design of high-speed inlets
By William C. Rose
Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees
Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees
By Ramadas K. Prabhu
Spectral solution of the viscous blunt body problem
Spectral solution of the viscous blunt body problem
By David A. Kopriva
Flow separation in shock wave boundary layer interactions at hypersonic speeds
Flow separation in shock wave boundary layer interactions at hypersonic speeds
By A. Hamed
On the Gortler vortex instability mechanism at hypersonic speeds
On the Gortler vortex instability mechanism at hypersonic speeds
By Philip Hall
Computational study of a McDonnell Douglas single-stage-to-orbit vehicle concept for aerodynamic analysis
Computational study of a McDonnell Douglas single-stage-to-orbit vehicle concept for aerodynamic analysis
By Ramadas K. Prabhu