Mach Number

136 books
Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnelRichard J. Re

Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel

Richard J. Re

1998No page data
Aeroacoustics of Low Mach Number FlowsWilliam Devenport
⏱ 9h 12m

Aeroacoustics of Low Mach Number Flows

William Devenport

2017552 pp.
Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63Jimmy L. Pittman
⏱ 1h 53m

Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63

Jimmy L. Pittman

1980113 pp.
Hypersonic pitching-moment shift for stardust reentry capsule forebodyWilliam A. Wood

Hypersonic pitching-moment shift for stardust reentry capsule forebody

William A. Wood

1997No page data
Aerodynamic tests of an AN-M-65-AZON 1000-pound radio-controlled bomb in the LMAL 16-foot high-speed tunnelLangley Aeronautical Laboratory
⏱ 1h 18m

Aerodynamic tests of an AN-M-65-AZON 1000-pound radio-controlled bomb in the LMAL 16-foot high-speed tunnel

Langley Aeronautical Laboratory

194478 pp.
Splitting methods for low Mach number Euler and Navier-Stokes equationsSaul S. Abarbanel

Splitting methods for low Mach number Euler and Navier-Stokes equations

Saul S. Abarbanel

1987No page data
Fuselage design for a specified Mach-sliced area distributionRaymond L. Barger

Fuselage design for a specified Mach-sliced area distribution

Raymond L. Barger

1990No page data
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 numbersSheryll Goecke Powers
⏱ 2h 19m

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

Sheryll Goecke Powers

1986139 pp.
Multigrid strategies for viscous flow solvers on anisotropic unstructured meshesDimitri Mavriplis

Multigrid strategies for viscous flow solvers on anisotropic unstructured meshes

Dimitri Mavriplis

1998No page data
The stability of two-dimensional wakes and shear-layers at high Mach numbersD. T. Papageorgiou

The stability of two-dimensional wakes and shear-layers at high Mach numbers

D. T. Papageorgiou

1990No page data
Flow coefficient behavior for boundary layer bleed holes and slotsB. P. Willis

Flow coefficient behavior for boundary layer bleed holes and slots

B. P. Willis

1995No page data
NASA Glenn 1-by 1-foot supersonic wind tunnel user manualUnknown Author

NASA Glenn 1-by 1-foot supersonic wind tunnel user manual

Unknown Author

1999No page data
NASA Glenn 1-by 1-foot supersonic wind tunnel user manualUnknown Author

NASA Glenn 1-by 1-foot supersonic wind tunnel user manual

Unknown Author

1999No page data
Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wingSheryll Goecke Powers

Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing

Sheryll Goecke Powers

1997No page data
The quest for mach oneChuck Yeager
⏱ 2h 22m

The quest for mach one

Chuck Yeager

1997142 pp.
Determination of sun angles for observations of shock waves on a transport aircraftUnknown Author

Determination of sun angles for observations of shock waves on a transport aircraft

Unknown Author

1998No page data
Fundamental study of flow field generated by rotorcraft bladesS. P. Parthasarathy

Fundamental study of flow field generated by rotorcraft blades

S. P. Parthasarathy

1985No page data
Near-optimal operation of dual-fuel launch vehiclesM. Ardema

Near-optimal operation of dual-fuel launch vehicles

M. Ardema

1996No page data
Porous and microporous honeycomb composites as potential boundary-layer bleed materialsD. O. Davis

Porous and microporous honeycomb composites as potential boundary-layer bleed materials

D. O. Davis

1997No page data
Experimental measurements of sonic boom signatures using a continuous data acquistion techniqueFloyd J. Wilcox
⏱ 45m

Experimental measurements of sonic boom signatures using a continuous data acquistion technique

Floyd J. Wilcox

201345 pp.
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