Boundary conditions and the simulation of low Mach number flows /

Analysis, approximation, and computation of a coupled solid/fluid temperature control problem /

Gunzburger, Max D.
Lee, Hyung C.
United States. National Aeronautics and Space Administration.

January 1993

"September 1993."Cover title.Includes bibliographical references (p. 31-32).Mode of access: Internet

Laminar flow transition : a large-eddy simulation /

Biringen, Sedat.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 34."February 1982"--Cover.Includes bibliographical references.Mode of access: Inter...

Investigation of the low-subsonic aerodynamic characteristics of a model of a modified lenticular reentry configuration /

Ware, George M.
Langley Research Center.

January 1962

"December 1962."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

On solving the compressible Navier-Stokes equations for unsteady flows at very low Mach numbers /

Pletcher, R. H.
Chen, K.-H.
United States. National Aeronautics and Space Administration.

January 1993

Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

Weak incident shock interactions with Mach 8 laminar boundary layers /

Kaufman, Louis G.
Johnson, Charles B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 21-23).Mode ...

Multigrid direct numerical simulation of the whole process of flow transition in 3-D boundary layers /

Liu, Chaoqun.
Liu, Zhining.
United States. National Aeronautics and Space Administration.

January 1993

"November 1993."Cover title.Includes bibliographical references (p. 37-38).Mode of access: Internet

Aerodynamic pressures and heating rates on surfaces between split elevons at Mach 6.6 /

Hunt, L. Roane (Lewis Roane)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"December 1988"--Cover.Includes bibliographical references (p. 13).Mode of access: Internet

Numerical studies of laminar and turbulent drag reduction : part II /

Balasubramanian, R. (Ramakrishna), 1945-
Orszag, Steven A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject Category 34."January 1983"--Cover.Includes bibliographical references.Mode of access: Intern...

Study of flow over oscillating airfoil models at a mach number of 7.0 in helium /

Arman, Ali
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Stresses and loads.Includes bibliographical references.Mode of access: I...

Experimental pressure distributions on a blunt lifting-entry body at Mach 3.71 /

Morris, W. Douglas.
Couch, Lana M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 12).Mode of access: Internet

Numerical boundary condition procedures : proceedings of a symposium held at NASA Ames Research Center, Moffett Field, California, October 19-20, 1981.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Ames Research Center.
Symposium on Numerical Boundary Condition Procedures (1981 : NASA Ames Research Center)

Item 830-H-10 (microfiche)."A collection of papers presented at the Symposium on Numerical Boundary ...

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...

Numerical calculations of two-dimensional, unsteady transonic flows with circulation /

Beam, Richard M.
Warming, Robert F. (Robert Fulton)
Ames Research Center.

January 1974

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 21-22).Mode of ...

Experimental and numerical investigation of boundary-layer development and transition on the walls of a Mach 5 nozzle /

Harvey, William D., 1934-
Harris, Julius E.
Cary, Aubrey M.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 23-25).Mode ...

Some problems of the calculation of three-dimensional boundary-layer flows on general configurations /

Cebeci, Tuncer.
Langley Research Center.
Douglas Aircraft Company.

January 1973

"Prepared by Douglas Aircraft Company, McDonnell Douglas Corporation ... for Langley Research Center...

Analysis, approximation, and computation of a coupled solid/fluid temperature control problem /

Gunzburger, Max D.
Lee, Hyung C.
United States. National Aeronautics and Space Administration.

January 1993

"September 1993."Cover title.Includes bibliographical references (p. 31-32).Mode of access: Internet

Laminar flow transition : a large-eddy simulation /

Biringen, Sedat.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 34."February 1982"--Cover.Includes bibliographical references.Mode of access: Inter...

Investigation of the low-subsonic aerodynamic characteristics of a model of a modified lenticular reentry configuration /

Ware, George M.
Langley Research Center.

January 1962

"December 1962."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

On solving the compressible Navier-Stokes equations for unsteady flows at very low Mach numbers /

Pletcher, R. H.
Chen, K.-H.
United States. National Aeronautics and Space Administration.

January 1993

Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

Weak incident shock interactions with Mach 8 laminar boundary layers /

Kaufman, Louis G.
Johnson, Charles B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 21-23).Mode ...

Multigrid direct numerical simulation of the whole process of flow transition in 3-D boundary layers /

Liu, Chaoqun.
Liu, Zhining.
United States. National Aeronautics and Space Administration.

January 1993

"November 1993."Cover title.Includes bibliographical references (p. 37-38).Mode of access: Internet

Aerodynamic pressures and heating rates on surfaces between split elevons at Mach 6.6 /

Hunt, L. Roane (Lewis Roane)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"December 1988"--Cover.Includes bibliographical references (p. 13).Mode of access: Internet

Numerical studies of laminar and turbulent drag reduction : part II /

Balasubramanian, R. (Ramakrishna), 1945-
Orszag, Steven A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject Category 34."January 1983"--Cover.Includes bibliographical references.Mode of access: Intern...

Study of flow over oscillating airfoil models at a mach number of 7.0 in helium /

Arman, Ali
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Stresses and loads.Includes bibliographical references.Mode of access: I...

Experimental pressure distributions on a blunt lifting-entry body at Mach 3.71 /

Morris, W. Douglas.
Couch, Lana M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 12).Mode of access: Internet

Numerical boundary condition procedures : proceedings of a symposium held at NASA Ames Research Center, Moffett Field, California, October 19-20, 1981.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Ames Research Center.
Symposium on Numerical Boundary Condition Procedures (1981 : NASA Ames Research Center)

Item 830-H-10 (microfiche)."A collection of papers presented at the Symposium on Numerical Boundary ...

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...

Numerical calculations of two-dimensional, unsteady transonic flows with circulation /

Beam, Richard M.
Warming, Robert F. (Robert Fulton)
Ames Research Center.

January 1974

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 21-22).Mode of ...

Experimental and numerical investigation of boundary-layer development and transition on the walls of a Mach 5 nozzle /

Harvey, William D., 1934-
Harris, Julius E.
Cary, Aubrey M.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 23-25).Mode ...

Some problems of the calculation of three-dimensional boundary-layer flows on general configurations /

Cebeci, Tuncer.
Langley Research Center.
Douglas Aircraft Company.

January 1973

"Prepared by Douglas Aircraft Company, McDonnell Douglas Corporation ... for Langley Research Center...

Analysis, approximation, and computation of a coupled solid/fluid temperature control problem /

Gunzburger, Max D.
Lee, Hyung C.
United States. National Aeronautics and Space Administration.

January 1993

"September 1993."Cover title.Includes bibliographical references (p. 31-32).Mode of access: Internet

Laminar flow transition : a large-eddy simulation /

Biringen, Sedat.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 34."February 1982"--Cover.Includes bibliographical references.Mode of access: Inter...

Investigation of the low-subsonic aerodynamic characteristics of a model of a modified lenticular reentry configuration /

Ware, George M.
Langley Research Center.

January 1962

"December 1962."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Boundary conditions and the simulation of low Mach number flows /

Abstract

Extracted data

Boundary conditions and the simulation of low Mach number flows /

Abstract

Extracted data

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