Hypersonic Flow

188 books
Application of electron beam fluorescence for characterization of hypersonic facility flowsW. Dan Williams
⏱ 16m

Application of electron beam fluorescence for characterization of hypersonic facility flows

W. Dan Williams

199216 pp.
Development and validation of an axisymmetric Navier-Stokes solver for hypersonic flowsR. Broglia
⏱ 43m

Development and validation of an axisymmetric Navier-Stokes solver for hypersonic flows

R. Broglia

199543 pp.
Prediction of L/D curves for a misssile in hypersonic flowClark, James W.
⏱ 1h 43m

Prediction of L/D curves for a misssile in hypersonic flow

Clark, James W.

1957103 pp.
Numerical simulations of unsteady flow in a hypersonic shock tunnel facilityJean-Luc Cambier
⏱ 23m

Numerical simulations of unsteady flow in a hypersonic shock tunnel facility

Jean-Luc Cambier

199223 pp.
Numerical simulation of hypersonic flow around a space plane. III Analysis of aerothermodynamic heatingYukimitsu Yamamoto
⏱ 28m

Numerical simulation of hypersonic flow around a space plane. III Analysis of aerothermodynamic heating

Yukimitsu Yamamoto

198928 pp.
An upwind parabolized Navier-Stokes code for real gas flowsJohn C. Tannehill
⏱ 12m

An upwind parabolized Navier-Stokes code for real gas flows

John C. Tannehill

198812 pp.
CW laser strategies for simultaneous multi-parameter measurements in high-speed gas flowsM. D. Di Rosa
⏱ 11m

CW laser strategies for simultaneous multi-parameter measurements in high-speed gas flows

M. D. Di Rosa

199211 pp.
A statistical theory for gas surface interactions in rarefied hypersonic flowsA. A. Agbormbai
⏱ 45m

A statistical theory for gas surface interactions in rarefied hypersonic flows

A. A. Agbormbai

198845 pp.
An upwind parabolized Navier-Stokes code for chemically reacting flowsJohn C. Tannehill
⏱ 13m

An upwind parabolized Navier-Stokes code for chemically reacting flows

John C. Tannehill

198813 pp.
Electron beam density measurement in a hypersonic shock tunnel flowfieldD. P. Shelton
⏱ 18m

Electron beam density measurement in a hypersonic shock tunnel flowfield

D. P. Shelton

199218 pp.
Shock-tunnel combustor testing for hypersonic vehiclesMark Loomis

Shock-tunnel combustor testing for hypersonic vehicles

Mark Loomis

1994No page data
Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D codeKamlesh Kapoor

Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code

Kamlesh Kapoor

1994No page data
Validation of WIND for a series of inlet flowsJohn W. Slater

Validation of WIND for a series of inlet flows

John W. Slater

2002No page data
High-order polynomial expansions (HOPE) for flux-vector splittingM. S. Liou

High-order polynomial expansions (HOPE) for flux-vector splitting

M. S. Liou

1991No page data
A study of the interaction of a laminar hypersonic boundary layer with a corner expansion waveAloysius Kou Fang Lo
⏱ 32m

A study of the interaction of a laminar hypersonic boundary layer with a corner expansion wave

Aloysius Kou Fang Lo

197032 pp.
The role of the turbulent viscous sublayer in the formation of surface patternsH. G. Lew
⏱ 1h 19m

The role of the turbulent viscous sublayer in the formation of surface patterns

H. G. Lew

196879 pp.
Hypersonic flows as related to the national aerospace planeMarvin Kussoy
⏱ 57m

Hypersonic flows as related to the national aerospace plane

Marvin Kussoy

199157 pp.
Discussions following the presentation of papers at the AGARD Fluid Dynamics Specialists' Meeting on "Separated flows"North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel.Specialists' Meeting
⏱ 42m

Discussions following the presentation of papers at the AGARD Fluid Dynamics Specialists' Meeting on "Separated flows"

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel.Specialists' Meeting

196642 pp.
Quantitative laser schlieren measurements in an expanding hypersonic laminar boundary layerWalter Wladislas Koziak

Quantitative laser schlieren measurements in an expanding hypersonic laminar boundary layer

Walter Wladislas Koziak

1971No page data
Separated flowsNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel. Specialists' Meeting
⏱ 16h 14m

Separated flows

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel. Specialists' Meeting

1966974 pp.
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