Local stability analysis for a planar shock wave /

Flight-measured laminar boundary layer transition phenomena including stability theory analysis /

Obara, Clifford J.
Holmes, Bruce J.
Langley Research Center.

January 1985

Prepared at Langley Research Center."April 1985"--Cover.Includes bibliographical references (p. 8).M...

Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack /

Satran, Dale R.
Anglin, Ernie L.
Gilbert, William P.
Langley Research Center.

January 1985

Prepared at Langley Research Center."May 1985"--Cover.Includes bibliographical references (p. 9-10)....

Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops /

Applin, Zachary T.
Coe, Paul L.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 63)....

Weak-wave analysis of shock interaction with a slipstream /

Barger, Raymond L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"November 1988"--Cover.Includes bibliographical references (p. 5-6).Mode of access: Internet

Dynamics of a one-dimensional plasma sheath /

Hohl, Frank.
Staton, Leo D.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."July 1968"--Cover.Includes bibliographical references (p. 32-33...

An analysis of shock coalescence including three-dimensional effects with application to sonic boom extrapolation /

Darden, Christine M.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Langley Research Center.

January 1984

"Langley Research Center.""January 1984"--Cover.Includes bibliographical references.Mode of access: ...

On the direct solution of the governing equation for radiation-resisted shock waves /

Pearson, Walter E.
Ames Research Center.

Prepared at Ames Research Center."January 1964"--Cover.Includes bibliographical references (p. 13).M...

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 ...

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...

Sonic-boom wave-front shapes and curvatures associated with maneuvering flight /

Barger, Raymond L.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject Category 02."December 1979"--Cover."Langley Research Center."Bibliography: p. 18.Mode of acc...

Investigation of a supersonic cruise fighter model flow field /

Reubush, David E.
Bare, E. Ann.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1985"--Cover.Includes bibliographical references (p. 8...

Flight test measurements and analysis of sonic boom phenomena near the shock wave extremity /

Haglund, George T. (George Thomas)
Kane, Edward J.
Langley Research Center.
Boeing Company.

January 1973

"Prepared by the Boeing Company ... for Langley Research Center."Cover title.Bibliography: p. 85-88....

Wind-tunnel investigation of the validity of a sonic-boom-minimization concept /

Mack, Robert J.
Darden, Christine M.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"Langley Research Center.""October 1979"--Cover.Includes bibliographical references.Mode of access: ...

Full-scale crash-test evaluation of two load-limiting subfloors for general aviation airframes /

Carden, Huey D.
Langley Research Center.

January 1984

Prepared at Langley Research Center."December 1984"--Cover.Includes bibliographical references (p. 1...

Semianalytic modeling of aerodynamic shapes /

Barger, Raymond L.
Adams, Mary S.
Langley Research Center.

January 1985

Prepared at Langley Research Center."April 1985"--Cover.Includes bibliographical references (p. 6).M...

Flight-measured laminar boundary layer transition phenomena including stability theory analysis /

Obara, Clifford J.
Holmes, Bruce J.
Langley Research Center.

January 1985

Prepared at Langley Research Center."April 1985"--Cover.Includes bibliographical references (p. 8).M...

Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack /

Satran, Dale R.
Anglin, Ernie L.
Gilbert, William P.
Langley Research Center.

January 1985

Prepared at Langley Research Center."May 1985"--Cover.Includes bibliographical references (p. 9-10)....

Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops /

Applin, Zachary T.
Coe, Paul L.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 63)....

Weak-wave analysis of shock interaction with a slipstream /

Barger, Raymond L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"November 1988"--Cover.Includes bibliographical references (p. 5-6).Mode of access: Internet

Dynamics of a one-dimensional plasma sheath /

Hohl, Frank.
Staton, Leo D.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."July 1968"--Cover.Includes bibliographical references (p. 32-33...

An analysis of shock coalescence including three-dimensional effects with application to sonic boom extrapolation /

Darden, Christine M.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Langley Research Center.

January 1984

"Langley Research Center.""January 1984"--Cover.Includes bibliographical references.Mode of access: ...

On the direct solution of the governing equation for radiation-resisted shock waves /

Pearson, Walter E.
Ames Research Center.

Prepared at Ames Research Center."January 1964"--Cover.Includes bibliographical references (p. 13).M...

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 ...

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...

Sonic-boom wave-front shapes and curvatures associated with maneuvering flight /

Barger, Raymond L.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject Category 02."December 1979"--Cover."Langley Research Center."Bibliography: p. 18.Mode of acc...

Investigation of a supersonic cruise fighter model flow field /

Reubush, David E.
Bare, E. Ann.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1985"--Cover.Includes bibliographical references (p. 8...

Flight test measurements and analysis of sonic boom phenomena near the shock wave extremity /

Haglund, George T. (George Thomas)
Kane, Edward J.
Langley Research Center.
Boeing Company.

January 1973

"Prepared by the Boeing Company ... for Langley Research Center."Cover title.Bibliography: p. 85-88....

Wind-tunnel investigation of the validity of a sonic-boom-minimization concept /

Mack, Robert J.
Darden, Christine M.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"Langley Research Center.""October 1979"--Cover.Includes bibliographical references.Mode of access: ...

Full-scale crash-test evaluation of two load-limiting subfloors for general aviation airframes /

Carden, Huey D.
Langley Research Center.

January 1984

Prepared at Langley Research Center."December 1984"--Cover.Includes bibliographical references (p. 1...

Semianalytic modeling of aerodynamic shapes /

Barger, Raymond L.
Adams, Mary S.
Langley Research Center.

January 1985

Prepared at Langley Research Center."April 1985"--Cover.Includes bibliographical references (p. 6).M...

Flight-measured laminar boundary layer transition phenomena including stability theory analysis /

Obara, Clifford J.
Holmes, Bruce J.
Langley Research Center.

January 1985

Prepared at Langley Research Center."April 1985"--Cover.Includes bibliographical references (p. 8).M...

Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack /

Satran, Dale R.
Anglin, Ernie L.
Gilbert, William P.
Langley Research Center.

January 1985

Prepared at Langley Research Center."May 1985"--Cover.Includes bibliographical references (p. 9-10)....

Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops /

Applin, Zachary T.
Coe, Paul L.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 63)....

Local stability analysis for a planar shock wave /

Abstract

Extracted data

Local stability analysis for a planar shock wave /

Abstract

Extracted data

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