Pressure distributions for a rectangular supersonic inlet at subsonic speeds /

Surface pressure distributions with a sonic jet normal to adjacent flat surfaces at Mach 2.92 to 6.4 /

Cubbison, Robert W.
Ward, James J.
Anderson, Bernhard H.
Lewis Research Center.

Prepared at Lewis Research Center."February 1961."Cover title.Includes bibliographical references (p...

Design and performance at a local Mach number of 6 of an inlet for an integrated scramjet concept /

Trexler, Carl A. (Carl Arthur), 1942-
Souders, Sue W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 50).Mode of ...

Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets /

Trefny, Charles J.
Wasserbauer, Joseph W.
Lewis Research Center.

January 1986

Prepared at Lewis Research Center."February 1986"--Cover.Includes bibliographical references (p. 10)...

Experimental cavity pressure distributions at supersonic speeds /

Stallings, Robert L.
Wilcox, Floyd J. (Floyd Jay)
Langley Research Center.

January 1987

Prepared at Langley Research Center."June 1987"--Cover.Includes bibliographical references (p. 9).Mo...

Pressure distribution on a vectored-thrust V/STOL fighter in the transition-speed range /

Mineck, Raymond E.
Margason, Richard J. (Richard John), 1936-
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Bibliography: p. 11.Mode of access: Internet

A short static-pressure probe design for supersonic flow /

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

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

Effect of subsonic inlet lip geometry on predicted surface and flow Mach number distributions /

Albers, James A.
Miller, Brent A.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ac...

Comparisons of theoretical and experimental pressure distributions over a wing-body model at high supersonic speeds /

Jernell, Lloyd S.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Prepared at Langley Research Center.N71-35197.Cover title.Includes bibliographical references (p. 8)...

Pressure distributions on a 1- by 3-meter semispan wing at sweep angles from 0 ̊to 40 ̊in subsonic flow /

Yip, Long P.
Shubert, l Gary L, joint author.
United States. National Aeronautics and Space Administration.

January 1976

Issued Dec. 1976.Includes bibliographical references (p. 9-10).Mode of access: Internet

Pressure distributions and shock shapes for 12.84/̊7 ̊on-axis and bent-nose biconics in air at mach 6 /

Miller, Charles G. (Charles George), 1940-
Gnoffo, Peter A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 02."December 1981"--Cover."Langley Research Center."Mode of access: Internet

Measured pressure distributions on large-angle cones in hypersonic flows of tetrafluoromethane, air, and helium /

Jones, Robert A.
Hunt, James L. (James Larry), 1939-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode ...

Analytical and experimental performance of optimal controller designs for a supersonic inlet /

Zeller, John R.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Bibliography: p. 84-85.Mode of access: Internet

Evaluation of some control-volume techniques for analysis of shock-boundary-layer interactions in supersonic inlets /

Hingst, Warren R.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 9).Mode of acc...

Pressure data for four analytically defined arrow wings in supersonic flow /

Townsend, James C. (James Courtland), 1938-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Sept. 1980."Langley Research Center."Bibliography: p. 16.Mode of access: Internet

Inlet spillage drag tests and numerical flow-field analysis at subsonic and transonic speeds of a 1/8-scale, two-dimensional, external-compression, variable-geometry supersonic inlet configuration /

Hawkins, J. E.
Turner, R. L. (Ralph Lilley), Sir, 1888-1983, joint author.
Kirkland, F. P., joint author.
Ames Research Center.
General Dynamics Corporation. Convair Aerospace Division.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 46).Mode of access: Internet

Surface pressure distributions with a sonic jet normal to adjacent flat surfaces at Mach 2.92 to 6.4 /

Cubbison, Robert W.
Ward, James J.
Anderson, Bernhard H.
Lewis Research Center.

Prepared at Lewis Research Center."February 1961."Cover title.Includes bibliographical references (p...

Design and performance at a local Mach number of 6 of an inlet for an integrated scramjet concept /

Trexler, Carl A. (Carl Arthur), 1942-
Souders, Sue W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 50).Mode of ...

Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets /

Trefny, Charles J.
Wasserbauer, Joseph W.
Lewis Research Center.

January 1986

Prepared at Lewis Research Center."February 1986"--Cover.Includes bibliographical references (p. 10)...

Experimental cavity pressure distributions at supersonic speeds /

Stallings, Robert L.
Wilcox, Floyd J. (Floyd Jay)
Langley Research Center.

January 1987

Prepared at Langley Research Center."June 1987"--Cover.Includes bibliographical references (p. 9).Mo...

Pressure distribution on a vectored-thrust V/STOL fighter in the transition-speed range /

Mineck, Raymond E.
Margason, Richard J. (Richard John), 1936-
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Bibliography: p. 11.Mode of access: Internet

A short static-pressure probe design for supersonic flow /

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

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

Effect of subsonic inlet lip geometry on predicted surface and flow Mach number distributions /

Albers, James A.
Miller, Brent A.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ac...

Comparisons of theoretical and experimental pressure distributions over a wing-body model at high supersonic speeds /

Jernell, Lloyd S.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Prepared at Langley Research Center.N71-35197.Cover title.Includes bibliographical references (p. 8)...

Pressure distributions on a 1- by 3-meter semispan wing at sweep angles from 0 ̊to 40 ̊in subsonic flow /

Yip, Long P.
Shubert, l Gary L, joint author.
United States. National Aeronautics and Space Administration.

January 1976

Issued Dec. 1976.Includes bibliographical references (p. 9-10).Mode of access: Internet

Pressure distributions and shock shapes for 12.84/̊7 ̊on-axis and bent-nose biconics in air at mach 6 /

Miller, Charles G. (Charles George), 1940-
Gnoffo, Peter A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 02."December 1981"--Cover."Langley Research Center."Mode of access: Internet

Measured pressure distributions on large-angle cones in hypersonic flows of tetrafluoromethane, air, and helium /

Jones, Robert A.
Hunt, James L. (James Larry), 1939-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode ...

Analytical and experimental performance of optimal controller designs for a supersonic inlet /

Zeller, John R.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Bibliography: p. 84-85.Mode of access: Internet

Evaluation of some control-volume techniques for analysis of shock-boundary-layer interactions in supersonic inlets /

Hingst, Warren R.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 9).Mode of acc...

Pressure data for four analytically defined arrow wings in supersonic flow /

Townsend, James C. (James Courtland), 1938-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Sept. 1980."Langley Research Center."Bibliography: p. 16.Mode of access: Internet

Inlet spillage drag tests and numerical flow-field analysis at subsonic and transonic speeds of a 1/8-scale, two-dimensional, external-compression, variable-geometry supersonic inlet configuration /

Hawkins, J. E.
Turner, R. L. (Ralph Lilley), Sir, 1888-1983, joint author.
Kirkland, F. P., joint author.
Ames Research Center.
General Dynamics Corporation. Convair Aerospace Division.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 46).Mode of access: Internet

Surface pressure distributions with a sonic jet normal to adjacent flat surfaces at Mach 2.92 to 6.4 /

Cubbison, Robert W.
Ward, James J.
Anderson, Bernhard H.
Lewis Research Center.

Prepared at Lewis Research Center."February 1961."Cover title.Includes bibliographical references (p...

Design and performance at a local Mach number of 6 of an inlet for an integrated scramjet concept /

Trexler, Carl A. (Carl Arthur), 1942-
Souders, Sue W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 50).Mode of ...

Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets /

Trefny, Charles J.
Wasserbauer, Joseph W.
Lewis Research Center.

January 1986

Prepared at Lewis Research Center."February 1986"--Cover.Includes bibliographical references (p. 10)...

Pressure distributions for a rectangular supersonic inlet at subsonic speeds /

Abstract

Extracted data

Pressure distributions for a rectangular supersonic inlet at subsonic speeds /

Abstract

Extracted data

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