Analytical method for predicting the pressure distribution about a nacelle at transonic speeds /

High-speed flow past wings /

Nørstrud, Helge, 1934-
Langley Research Center.
Lockheed-Georgia Company.

January 1973

"Prepared by Lockheed-Georgia Company ... for Langley Research Center."Cover title.Bibliography: p. ...

Transonic pressure distributions over protuberances and adjacent areas in proximity to the nose of a launch vehicle /

Blackwell, James A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1966

Cover title."March 1966."Includes bibliographical references (p. 7).Mode of access: Internet

Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wing /

Keener, Earl R.
Flight Research Center (U.S.)

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 14-15).Mode of access: Internet

Method to predict external store carriage characteristics at transonic speeds / Bruce S. Rosen.

Rosen, Bruce S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

Prepared for Langley Research Center under Contract NAS1-18105."August 1988"--Cover.Bibliography: p....

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

Pressure distributions for a rectangular supersonic inlet at subsonic speeds /

Fuller, Dennis E.
Langley Research Center.

January 1976

Research prepared at Langley Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

An analysis of the pressure distribution measured on a body of revolution at transonic speeds in the slotted test section of the Langley 8-foot transonic tunnel /

Estabrooks, Bruce B.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"June 25, 1952."Includes bibliographical references (p. 23).Mode of access: Internet

Calculation of the twist distribution of wings designed for cruise at transonic speeds /

Mann, Michael J.
Langley Research Center.

January 1974

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

Development of a nonlinear unsteady transonic flow theory /

Stahara, Stephen S.
Spreiter, John R.
Langley Research Center.
Nielsen Engineering & Research.

January 1973

"Prepared by Nielsen Engineering & Research, Inc. ... for Langley Research Center."Cover title.Bibli...

Elastohydrodynamic analysis using a power law pressure-viscosity relation /

Loewenthal, Stuart H.
Zaretsky, Erwin V.
U.S. Army Air Mobility Research and Development Laboratory.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center and the U.S. Army Air Mobility R&D Laboratory.Cover title.Bibliogr...

Numerical calculations of velocity and pressure distribution around oscillating airfoils /

Bratanow, Theodore.
Kobiske, Michael.
Ecer, Akin.
Langley Research Center.
University of Wisconsin--Milwaukee.

January 1974

"Prepared by University of Wisconsin-Milwaukee ... for Langley Research Center."Cover title.Bibliogr...

Analysis of transonic flow about lifting wing-body configurations /

Barnwell, Richard W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

Description and calibration of the Langley 6- by 19-inch transonic tunnel /

Ladson, Charles L.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 16-17.Mode of access: Internet

Pressure measurements of the leading edge of a swept wing at Mach 2.2 /

Sorrells, Russell B.
Langley Research Center.

January 1974

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

A method for predicting shock shapes and pressure distributions on two-dimensional airfoils at large angles of attack /

Kaattari, George E.
Ames Research Center.

January 1973

Prepared at Ames Research Center.Cover title.Bibliography: p. 28.Mode of access: Internet

High-speed flow past wings /

Nørstrud, Helge, 1934-
Langley Research Center.
Lockheed-Georgia Company.

January 1973

"Prepared by Lockheed-Georgia Company ... for Langley Research Center."Cover title.Bibliography: p. ...

Transonic pressure distributions over protuberances and adjacent areas in proximity to the nose of a launch vehicle /

Blackwell, James A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1966

Cover title."March 1966."Includes bibliographical references (p. 7).Mode of access: Internet

Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wing /

Keener, Earl R.
Flight Research Center (U.S.)

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 14-15).Mode of access: Internet

Method to predict external store carriage characteristics at transonic speeds / Bruce S. Rosen.

Rosen, Bruce S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

Prepared for Langley Research Center under Contract NAS1-18105."August 1988"--Cover.Bibliography: p....

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

Pressure distributions for a rectangular supersonic inlet at subsonic speeds /

Fuller, Dennis E.
Langley Research Center.

January 1976

Research prepared at Langley Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

An analysis of the pressure distribution measured on a body of revolution at transonic speeds in the slotted test section of the Langley 8-foot transonic tunnel /

Estabrooks, Bruce B.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"June 25, 1952."Includes bibliographical references (p. 23).Mode of access: Internet

Calculation of the twist distribution of wings designed for cruise at transonic speeds /

Mann, Michael J.
Langley Research Center.

January 1974

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

Development of a nonlinear unsteady transonic flow theory /

Stahara, Stephen S.
Spreiter, John R.
Langley Research Center.
Nielsen Engineering & Research.

January 1973

"Prepared by Nielsen Engineering & Research, Inc. ... for Langley Research Center."Cover title.Bibli...

Elastohydrodynamic analysis using a power law pressure-viscosity relation /

Loewenthal, Stuart H.
Zaretsky, Erwin V.
U.S. Army Air Mobility Research and Development Laboratory.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center and the U.S. Army Air Mobility R&D Laboratory.Cover title.Bibliogr...

Numerical calculations of velocity and pressure distribution around oscillating airfoils /

Bratanow, Theodore.
Kobiske, Michael.
Ecer, Akin.
Langley Research Center.
University of Wisconsin--Milwaukee.

January 1974

"Prepared by University of Wisconsin-Milwaukee ... for Langley Research Center."Cover title.Bibliogr...

Analysis of transonic flow about lifting wing-body configurations /

Barnwell, Richard W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

Description and calibration of the Langley 6- by 19-inch transonic tunnel /

Ladson, Charles L.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 16-17.Mode of access: Internet

Pressure measurements of the leading edge of a swept wing at Mach 2.2 /

Sorrells, Russell B.
Langley Research Center.

January 1974

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

A method for predicting shock shapes and pressure distributions on two-dimensional airfoils at large angles of attack /

Kaattari, George E.
Ames Research Center.

January 1973

Prepared at Ames Research Center.Cover title.Bibliography: p. 28.Mode of access: Internet

High-speed flow past wings /

Nørstrud, Helge, 1934-
Langley Research Center.
Lockheed-Georgia Company.

January 1973

"Prepared by Lockheed-Georgia Company ... for Langley Research Center."Cover title.Bibliography: p. ...

Transonic pressure distributions over protuberances and adjacent areas in proximity to the nose of a launch vehicle /

Blackwell, James A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1966

Cover title."March 1966."Includes bibliographical references (p. 7).Mode of access: Internet

Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wing /

Keener, Earl R.
Flight Research Center (U.S.)

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 14-15).Mode of access: Internet

Analytical method for predicting the pressure distribution about a nacelle at transonic speeds /

Abstract

Extracted data

Analytical method for predicting the pressure distribution about a nacelle at transonic speeds /

Abstract

Extracted data

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