Solutions of blunt-body stagnation-region flows with nongray emission and absorption of radiation by a time-asymptotic technique /

Thin radiating shock layer about a blunt body /

Chou, Y. S.
Blake, L. H.
Ames Research Center.
Lockheed Aircraft Corporation.

January 1970

Boundary layer flow in thin shock layer about axisymmetric blunt bodies studied by Blasius type seri...

Observations on the flows past blunt bodies at transonic speeds /

Everhart, Philip E.
Lindsey, Walter F.
United States. National Aeronautics and Space Administration.

"1960."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Hypersonic ionizing air viscous shock-layer flows over nonanalytic blunt bodies /

Miner. E. W. (Earnest Wade), 1941-
Lewis, Clark H.
Lyndon B. Johnson Space Center.
Virginia Polytechnic Institute and State University. Aerospace and Ocean Engineering Dept.

"Prepared by Virginia Polytechnic Institute and State University, [Aerospace and Ocean Engineering D...

A method of integral relations solution for radiating, nonadiabatic, inviscid flow over a blunt body /

Suttles, John T. (John Timothy)
Langley Research Center.

Prepared at Langley Research Center."October 1969."Cover title.Includes bibliographical references (...

An approximate analysis of unsteady vaporization near the stagnation point of blunt bodies /

Roberts, Leonard.
Langley Research Center.

January 1959

"NASA TN D-41.""Langley Research Center, Langley Field, Va.""September 1959."Title from cover.Includ...

Radiation emission effects of the equilibrium boundary layer in the stagnation region /

Howe, John Thomas.
United States. National Aeronautics and Space Administration.

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

Blunt body stagnation region flow with nongray radiation heat transfer - A singular perturbation solution

Olstad, W. B.

November 1968

Perturbation solution to blunt body stagnation region flow of radiating gas with radiation heat tran...

A program for equilibrium normal shock and stagnation point solutions for arbitrary gas mixtures /

Callis, Linwood B.
Kemper, Jane T.
Langley Research Center.

Prepared at Langley Research Center."February 1966"--Cover.Includes bibliographical references (p. 5...

An approximate analysis of film cooling on blunt bodies by gas injection near the stagnation point. /

Swenson, Byron L.
United States. National Aeronautics and Space Administration.

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

Inviscid hypersonic flow over a blunt body with high rates of mass and heat transfer /

Martin, E. Dale (Elmer Dale)
Ames Research Center.

Prepared at Ames Research Center."March 1968"--Cover.Includes bibliographical references (p. 30-31)....

Effect of localized mass transfer near the stagnation region of blunt bodies in hypersonic flight /

Chung, Paul M. (Paul Myung-Ha)
Ames Research Center.

January 1959

"NASA TN D-141.""Ames Research Center, Moffett Field, Calif.""May 1960."Title from cover.Includes bi...

Regime of frozen boundary layers in stagnation region of blunt reentry bodies /

Grier, Norman T.
Sands, Norman.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, missiles and space vehicles; Atmospheric entry' Fluid mechanics...

Calculation of axisymmetric supersonic flow past blunt bodies with sonic corners : including a program description and listing /

South, Jerry C. (Jerry Curtis), 1935-
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 36-37).Mode of access: Internet

Semiempirical method for predicting effects of incident-reflecting shocks on the turbulent boundary layer /

Pinckney, S. Z. (Shimer Zane), 1934-
Langley Research Center.

Prepared at Langley Research Center."October 1965"--Cover.Includes bibliographical references (p. 38...

A semiempirical collision model for plasmas /

Meador, Willard E.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."May 1969"--Cover.Includes bibliographical references (p. 32).Mo...

Thin radiating shock layer about a blunt body /

Chou, Y. S.
Blake, L. H.
Ames Research Center.
Lockheed Aircraft Corporation.

January 1970

Boundary layer flow in thin shock layer about axisymmetric blunt bodies studied by Blasius type seri...

Observations on the flows past blunt bodies at transonic speeds /

Everhart, Philip E.
Lindsey, Walter F.
United States. National Aeronautics and Space Administration.

"1960."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Hypersonic ionizing air viscous shock-layer flows over nonanalytic blunt bodies /

Miner. E. W. (Earnest Wade), 1941-
Lewis, Clark H.
Lyndon B. Johnson Space Center.
Virginia Polytechnic Institute and State University. Aerospace and Ocean Engineering Dept.

"Prepared by Virginia Polytechnic Institute and State University, [Aerospace and Ocean Engineering D...

A method of integral relations solution for radiating, nonadiabatic, inviscid flow over a blunt body /

Suttles, John T. (John Timothy)
Langley Research Center.

Prepared at Langley Research Center."October 1969."Cover title.Includes bibliographical references (...

An approximate analysis of unsteady vaporization near the stagnation point of blunt bodies /

Roberts, Leonard.
Langley Research Center.

January 1959

"NASA TN D-41.""Langley Research Center, Langley Field, Va.""September 1959."Title from cover.Includ...

Radiation emission effects of the equilibrium boundary layer in the stagnation region /

Howe, John Thomas.
United States. National Aeronautics and Space Administration.

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

Blunt body stagnation region flow with nongray radiation heat transfer - A singular perturbation solution

Olstad, W. B.

November 1968

Perturbation solution to blunt body stagnation region flow of radiating gas with radiation heat tran...

A program for equilibrium normal shock and stagnation point solutions for arbitrary gas mixtures /

Callis, Linwood B.
Kemper, Jane T.
Langley Research Center.

Prepared at Langley Research Center."February 1966"--Cover.Includes bibliographical references (p. 5...

An approximate analysis of film cooling on blunt bodies by gas injection near the stagnation point. /

Swenson, Byron L.
United States. National Aeronautics and Space Administration.

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

Inviscid hypersonic flow over a blunt body with high rates of mass and heat transfer /

Martin, E. Dale (Elmer Dale)
Ames Research Center.

Prepared at Ames Research Center."March 1968"--Cover.Includes bibliographical references (p. 30-31)....

Effect of localized mass transfer near the stagnation region of blunt bodies in hypersonic flight /

Chung, Paul M. (Paul Myung-Ha)
Ames Research Center.

January 1959

"NASA TN D-141.""Ames Research Center, Moffett Field, Calif.""May 1960."Title from cover.Includes bi...

Regime of frozen boundary layers in stagnation region of blunt reentry bodies /

Grier, Norman T.
Sands, Norman.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, missiles and space vehicles; Atmospheric entry' Fluid mechanics...

Calculation of axisymmetric supersonic flow past blunt bodies with sonic corners : including a program description and listing /

South, Jerry C. (Jerry Curtis), 1935-
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 36-37).Mode of access: Internet

Semiempirical method for predicting effects of incident-reflecting shocks on the turbulent boundary layer /

Pinckney, S. Z. (Shimer Zane), 1934-
Langley Research Center.

Prepared at Langley Research Center."October 1965"--Cover.Includes bibliographical references (p. 38...

A semiempirical collision model for plasmas /

Meador, Willard E.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."May 1969"--Cover.Includes bibliographical references (p. 32).Mo...

Thin radiating shock layer about a blunt body /

Chou, Y. S.
Blake, L. H.
Ames Research Center.
Lockheed Aircraft Corporation.

January 1970

Boundary layer flow in thin shock layer about axisymmetric blunt bodies studied by Blasius type seri...

Observations on the flows past blunt bodies at transonic speeds /

Everhart, Philip E.
Lindsey, Walter F.
United States. National Aeronautics and Space Administration.

"1960."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Hypersonic ionizing air viscous shock-layer flows over nonanalytic blunt bodies /

Miner. E. W. (Earnest Wade), 1941-
Lewis, Clark H.
Lyndon B. Johnson Space Center.
Virginia Polytechnic Institute and State University. Aerospace and Ocean Engineering Dept.

"Prepared by Virginia Polytechnic Institute and State University, [Aerospace and Ocean Engineering D...

Solutions of blunt-body stagnation-region flows with nongray emission and absorption of radiation by a time-asymptotic technique /

Abstract

Extracted data

Solutions of blunt-body stagnation-region flows with nongray emission and absorption of radiation by a time-asymptotic technique /

Abstract

Extracted data

Related items

Related items