1-24 of 116 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
Hypersonic pitching-moment shift for stardust reentry capsule forebody
Hypersonic pitching-moment shift for stardust reentry capsule forebody
By William A. Wood
User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel
User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel
By Ronald H. Soeder
F-18 High Alpha Research Vehicle surface pressures
F-18 High Alpha Research Vehicle surface pressures
By David F. Fisher
High-resolution shock capturing scheme for high Mach number internal flow
High-resolution shock capturing scheme for high Mach number internal flow
By Seokkwan Yoon
Near-optimal operation of dual-fuel launch vehicles
Near-optimal operation of dual-fuel launch vehicles
By M. Ardema
Progress in Favré-Reynolds stress closures for compressible flows
Progress in Favré-Reynolds stress closures for compressible flows
By V. Adumitroaie
Flow-separation patterns on symmetric forebodies
Flow-separation patterns on symmetric forebodies
By Earl R. Keener
Euler/Navier-Stokes flow computations on flexible configurations for stability analysis
Euler/Navier-Stokes flow computations on flexible configurations for stability analysis
By G. Guruswamy
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
Numerical simulation of the generation of axisymmetric mode jet screech tones
Numerical simulation of the generation of axisymmetric mode jet screech tones
By Hao Shen
Consistent initial conditions for the DNS of compressible turbulence
Consistent initial conditions for the DNS of compressible turbulence
By J. R. Ristorcelli
Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers
Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers
By Sheryll Goecke Powers
In-flight transition measurement on a 10
In-flight transition measurement on a 10
By David F. Fisher
Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20
Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20
By Lawrence E. Putnam
The stability of two-dimensional wakes and shear-layers at high Mach numbers
The stability of two-dimensional wakes and shear-layers at high Mach numbers
By D. T. Papageorgiou
Control of unsteady separated flow associated with the dynamic stall of airfoils
Control of unsteady separated flow associated with the dynamic stall of airfoils
By Michael C. Wilder
High-lift flight tunnel
High-lift flight tunnel
By David Lofftus
Aeroacoustics of Low Mach Number Flows
Aeroacoustics of Low Mach Number Flows
By William Devenport,Stewart Glegg
Shock-tunnel combustor testing for hypersonic vehicles
Shock-tunnel combustor testing for hypersonic vehicles
By Mark Loomis
Comparison of the aeroacoustics of two small-scale supersonic inlets
Comparison of the aeroacoustics of two small-scale supersonic inlets
By Wing Ng
Performance of the 0.3-meter transonic cryogenic tunnel with air, nitrogen, and sulfer hexafluoride media under closed loop automatic control
Performance of the 0.3-meter transonic cryogenic tunnel with air, nitrogen, and sulfer hexafluoride media under closed loop automatic control
By Balakrishna, S.
Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
By John W. Edwards
Supersonic symposium
Supersonic symposium
By Supersonic Symposium (1987 Edwards Air Force Base, Calif.)