Stability of three-dimensional compressible boundary layers /

Transonic pressure distributions on three rigid wings simulating paragliders with varied canopy curvature and leading edge sweep /

Fournier, Paul G.
Bell, B. Ann.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircra...

On the flow structure within a constant pressure compressible turbulent jet mixing region /

Chow, W. L.
Korst, H. H.
United States. National Aeronautics and Space Administration.

Cover title."April 1963."Includes bibliographical references.Mode of access: Internet

Charts for air flow properties in equilibrium and frozen flows in hypervelocity nozzles /

Yoshikawa, Kenneth K.
Katzen, Elliott D.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics; Propulsion syst...

Some simple solutions to the problem of predicting boundary-layer self-induced pressures /

Bertram, Michael H.
Blackstock, Thomas A.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid me...

Analysis of melting boundary layers on decelerating bodies /

Ostrach, Simon.
Hamman, Jesse.
Goldstein, Arthur W.
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanic...

Secondary flow fields embedded in hypersonic shock layers /

Seiff, Alvin.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Stability and con...

The compressible turbulent boundary layer on a blunt swept slab with and without leading-edge blowing /

Hunt, James L. (James Larry), 1939-
Beckwith, Ivan E.
Bushnell, Dennis M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."March 1971."Cover title.Includes bibliographical references (p....

Effects of mach number, leading edge bluntness and sweep on boundary-layer transition on a flat plate /

Jillie, Don W.
Hopkins, Edward J.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bib...

A general method for calculating three-dimensional compressible laminar and turbulent boundary layers on arbitrary wings /

Cebeci, Tuncer.
Ramsey, Judy A., joint author.
Kaups, Kalle, joint author.
McDonnell Douglas Corporation.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1977

Issued Jan. 1977.Prepared by McDonnell Douglas Corporation for Langley Research Center under NAS1-12...

The blunt plate in hypersonic flow /

Baradell, Donald L. (Donald Louis), 1933-
Bertram, Mitchel H.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid ...

Numerical solutions for supersonic flow of an ideal gas around blunt two-dimensional bodies /

Fuller, Franklyn B.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid mec...

Boundary-layer transition on a group of blunt nose shapes at a mach number of 2.20 /

Jackson, Mary W.
Czatnecki, K. R.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Major NASA subject terms: Aerodynamics, aircraft; Aerodynamics, missiles and...

Some effects of leading-edge sweep on boundary-layer transition at supersonic speeds /

Chapman, Gary T.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Flui...

Aerodynamics of a tilting ducted fan configuration /

Yaggy, Paul F.
Goodson, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet; Stability an...

Low-subsonic-speed static stability of right-triangular-pyramid and half-cone lifting reentry configurations. /

Ware, George M.
United States. National Aeronautics and Space Administration.

Abstract:Cover title."February 1961."Aerodynamics, missiles and space vehicles; Space vehicles; Stab...

Transonic pressure distributions on three rigid wings simulating paragliders with varied canopy curvature and leading edge sweep /

Fournier, Paul G.
Bell, B. Ann.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircra...

On the flow structure within a constant pressure compressible turbulent jet mixing region /

Chow, W. L.
Korst, H. H.
United States. National Aeronautics and Space Administration.

Cover title."April 1963."Includes bibliographical references.Mode of access: Internet

Charts for air flow properties in equilibrium and frozen flows in hypervelocity nozzles /

Yoshikawa, Kenneth K.
Katzen, Elliott D.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics; Propulsion syst...

Some simple solutions to the problem of predicting boundary-layer self-induced pressures /

Bertram, Michael H.
Blackstock, Thomas A.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid me...

Analysis of melting boundary layers on decelerating bodies /

Ostrach, Simon.
Hamman, Jesse.
Goldstein, Arthur W.
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanic...

Secondary flow fields embedded in hypersonic shock layers /

Seiff, Alvin.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Stability and con...

The compressible turbulent boundary layer on a blunt swept slab with and without leading-edge blowing /

Hunt, James L. (James Larry), 1939-
Beckwith, Ivan E.
Bushnell, Dennis M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."March 1971."Cover title.Includes bibliographical references (p....

Effects of mach number, leading edge bluntness and sweep on boundary-layer transition on a flat plate /

Jillie, Don W.
Hopkins, Edward J.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bib...

A general method for calculating three-dimensional compressible laminar and turbulent boundary layers on arbitrary wings /

Cebeci, Tuncer.
Ramsey, Judy A., joint author.
Kaups, Kalle, joint author.
McDonnell Douglas Corporation.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1977

Issued Jan. 1977.Prepared by McDonnell Douglas Corporation for Langley Research Center under NAS1-12...

The blunt plate in hypersonic flow /

Baradell, Donald L. (Donald Louis), 1933-
Bertram, Mitchel H.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid ...

Numerical solutions for supersonic flow of an ideal gas around blunt two-dimensional bodies /

Fuller, Franklyn B.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid mec...

Boundary-layer transition on a group of blunt nose shapes at a mach number of 2.20 /

Jackson, Mary W.
Czatnecki, K. R.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Major NASA subject terms: Aerodynamics, aircraft; Aerodynamics, missiles and...

Some effects of leading-edge sweep on boundary-layer transition at supersonic speeds /

Chapman, Gary T.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Flui...

Aerodynamics of a tilting ducted fan configuration /

Yaggy, Paul F.
Goodson, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet; Stability an...

Low-subsonic-speed static stability of right-triangular-pyramid and half-cone lifting reentry configurations. /

Ware, George M.
United States. National Aeronautics and Space Administration.

Abstract:Cover title."February 1961."Aerodynamics, missiles and space vehicles; Space vehicles; Stab...

Transonic pressure distributions on three rigid wings simulating paragliders with varied canopy curvature and leading edge sweep /

Fournier, Paul G.
Bell, B. Ann.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircra...

On the flow structure within a constant pressure compressible turbulent jet mixing region /

Chow, W. L.
Korst, H. H.
United States. National Aeronautics and Space Administration.

Cover title."April 1963."Includes bibliographical references.Mode of access: Internet

Charts for air flow properties in equilibrium and frozen flows in hypervelocity nozzles /

Yoshikawa, Kenneth K.
Katzen, Elliott D.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics; Propulsion syst...

Stability of three-dimensional compressible boundary layers /

Abstract

Extracted data

Stability of three-dimensional compressible boundary layers /

Abstract

Extracted data

Related items

Related items