1-24 of 25 Books
Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration
Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration
By W. Pelham Phillips
Navier-Stokes simulation of several high-lift reference H configurations
Navier-Stokes simulation of several high-lift reference H configurations
By Wendy B. Lessard
Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel
Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel
By Richard J. Re
Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction
Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction
By Aerospace Sciences Meeting & Exhibit (32nd 1994 Reno, Nev.)
Preliminary airborne measurements for the SR-71 sonic boom propagation experiment
Preliminary airborne measurements for the SR-71 sonic boom propagation experiment
By Edward A. Haering
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
Flow coefficient behavior for boundary layer bleed holes and slots
Flow coefficient behavior for boundary layer bleed holes and slots
By B. P. Willis
Lee-side flow over delta wings at supersonic speeds
Lee-side flow over delta wings at supersonic speeds
By David S. Miller
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
First order ozone impact of a fleet of supersonic business jets (SSBJs)
First order ozone impact of a fleet of supersonic business jets (SSBJs)
By Steven L. Baughcum
Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight
Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight
By Scott R. Thomas
Control effectiveness and tip-fin dihedral effects for the HL-20 lifting-body configuration at Mach numbers from 1.6 to 4.5
Control effectiveness and tip-fin dihedral effects for the HL-20 lifting-body configuration at Mach numbers from 1.6 to 4.5
By Christopher I. Cruz
Lee-side flow over delta wings at supersonic speeds
Lee-side flow over delta wings at supersonic speeds
By D. S. Miller
Concept development of a Mach 2.4 high-speed civil transport
Concept development of a Mach 2.4 high-speed civil transport
By Langley Research Center
Simulation of crossflow instability on a supersonic highly swept wing
Simulation of crossflow instability on a supersonic highly swept wing
By C. David Pruett
High speed commercial transport fuels considerations and research needs
High speed commercial transport fuels considerations and research needs
By C. M. Lee
Computations of axisymmetric flows in hypersonic shock tubes
Computations of axisymmetric flows in hypersonic shock tubes
By Surendra P. Sharma
Effect of milling machine roughness and wing dihedral on the supersonic aerodynamic characteristics of a highly swept wing
Effect of milling machine roughness and wing dihedral on the supersonic aerodynamic characteristics of a highly swept wing
By Christine M. Darden
Parametric study on laminar flow for finite wings at supersonic speeds
Parametric study on laminar flow for finite wings at supersonic speeds
By Joseph Avila Garcia
Nonlinear potential analysis techniques for supersonic/hypersonic aerodynamic design
Nonlinear potential analysis techniques for supersonic/hypersonic aerodynamic design
By V. Shankar
Preliminary measurement of the noise from the 2/9 scale model of the large-scale advanced propfan (LAP) propeller, SR-7A
Preliminary measurement of the noise from the 2/9 scale model of the large-scale advanced propfan (LAP) propeller, SR-7A
By James H. Dittmar
Experimental study at low supersonic speeds of a missile concept having opposing wraparound tails
Experimental study at low supersonic speeds of a missile concept having opposing wraparound tails
By Jerry M. Allen
Effect of density gradients in confined supersonic shear layers
Effect of density gradients in confined supersonic shear layers
By Oshin Peroomian