Water landing characteristics of a model of a winged reentry vehicle /

Model investigation of the landing characteristics of a reentry spacecraft with a vertical-cylinder air bag for load alleviation /

McGehee, John R.
Vaughan, Victor L.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, missiles and space vehicles; Space vehicles.Includes bibliogr...

Theoretical and experimental studies of reentry plasmas /

Dunn, M. G. (Michael G.)
Kang, Sang-Wook.
Langley Research Center.
Cornell Aeronautical Laboratory.

January 1973

"Prepared by Cornell Aeronautical Laboratory ... for Langley Research Center."Cover title.Bibliograp...

Low-speed aerodynamic characteristics of an airfoil optimized for maximum lift coefficient /

Bingham, Gene J.
Chen, Allen Wen-shin, 1945-
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 13.Mode of access: Internet

Landing-impact studies of a 0.3-scale model air cushion landing system for a Navy fighter airplane /

Leland, Trafford J. W.
Thompson, William C. (William Crawford)
Langley Research Center.

January 1975

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

Water-landing characteristics of a 1/10-scale model of a winged missile /

Fisher, Lloyd J.
United States. National Aeronautics and Space Administration.

Cover title."April 1967."Includes bibliographical references.Mode of access: Internet

Simulation of decelerating landing approaches on an externally blown flap STOL transport airplane /

Grantham, William D.
Deal, Perry L.
Nguyen, Luat T.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 19).Mode of ...

Flight investigation of manual and automatic VTOL decelerating instrument approaches and landings /

Kelly, James R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Bibliography: p. 22.Mode of access: Internet

Experimental validation of a landing-dynamics computer program for legged spacecraft landers /

McGehee, John R.
Stubbs, Sandy M.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 42-43.Mode of access: Internet

Flight-determined derivatives and dynamic characteristics of the CV-990 airplane /

Gilyard, Glenn B.
Flight Research Center (U.S.)

January 1972

Prepared at NASA Flight Research Center.Cover title.Bibliography: p. 24.Mode of access: Internet

Effect of Reynolds number and engine nacelles on the stalling characteristics of a model of a twin-engine light airplane /

Lockwood, Vernard E.
Langley Research Center.

January 1972

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

Investigation of the landing characteristics of a reentry vehicle having a canted multiple-air-bag load-alleviation system /

Stubbs, Sandy M.
McGehee, John R.
United States. National Aeronautics and Space Administration.

Cover title."August 1963."Includes bibliographical references.Mode of access: Internet

Automatic guidance and control of a transport aircraft during a helical landing approach /

Crawford, Daniel J.
Bowles, Roland L.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 35).Mode of ...

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

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

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. ...

Consideration of some aerodynamic characteristics during take-off and landing of jet airplanes /

Riebe, John M.
Langley Research Center.

January 1959

"NASA TN D-19.""Langley Research Center, Langley Field, Va.""September 1959."Cover title.Mode of acc...

Model investigation of the landing characteristics of a reentry spacecraft with a vertical-cylinder air bag for load alleviation /

McGehee, John R.
Vaughan, Victor L.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, missiles and space vehicles; Space vehicles.Includes bibliogr...

Theoretical and experimental studies of reentry plasmas /

Dunn, M. G. (Michael G.)
Kang, Sang-Wook.
Langley Research Center.
Cornell Aeronautical Laboratory.

January 1973

"Prepared by Cornell Aeronautical Laboratory ... for Langley Research Center."Cover title.Bibliograp...

Low-speed aerodynamic characteristics of an airfoil optimized for maximum lift coefficient /

Bingham, Gene J.
Chen, Allen Wen-shin, 1945-
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 13.Mode of access: Internet

Landing-impact studies of a 0.3-scale model air cushion landing system for a Navy fighter airplane /

Leland, Trafford J. W.
Thompson, William C. (William Crawford)
Langley Research Center.

January 1975

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

Water-landing characteristics of a 1/10-scale model of a winged missile /

Fisher, Lloyd J.
United States. National Aeronautics and Space Administration.

Cover title."April 1967."Includes bibliographical references.Mode of access: Internet

Simulation of decelerating landing approaches on an externally blown flap STOL transport airplane /

Grantham, William D.
Deal, Perry L.
Nguyen, Luat T.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 19).Mode of ...

Flight investigation of manual and automatic VTOL decelerating instrument approaches and landings /

Kelly, James R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Bibliography: p. 22.Mode of access: Internet

Experimental validation of a landing-dynamics computer program for legged spacecraft landers /

McGehee, John R.
Stubbs, Sandy M.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 42-43.Mode of access: Internet

Flight-determined derivatives and dynamic characteristics of the CV-990 airplane /

Gilyard, Glenn B.
Flight Research Center (U.S.)

January 1972

Prepared at NASA Flight Research Center.Cover title.Bibliography: p. 24.Mode of access: Internet

Effect of Reynolds number and engine nacelles on the stalling characteristics of a model of a twin-engine light airplane /

Lockwood, Vernard E.
Langley Research Center.

January 1972

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

Investigation of the landing characteristics of a reentry vehicle having a canted multiple-air-bag load-alleviation system /

Stubbs, Sandy M.
McGehee, John R.
United States. National Aeronautics and Space Administration.

Cover title."August 1963."Includes bibliographical references.Mode of access: Internet

Automatic guidance and control of a transport aircraft during a helical landing approach /

Crawford, Daniel J.
Bowles, Roland L.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 35).Mode of ...

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

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

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. ...

Consideration of some aerodynamic characteristics during take-off and landing of jet airplanes /

Riebe, John M.
Langley Research Center.

January 1959

"NASA TN D-19.""Langley Research Center, Langley Field, Va.""September 1959."Cover title.Mode of acc...

Model investigation of the landing characteristics of a reentry spacecraft with a vertical-cylinder air bag for load alleviation /

McGehee, John R.
Vaughan, Victor L.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, missiles and space vehicles; Space vehicles.Includes bibliogr...

Theoretical and experimental studies of reentry plasmas /

Dunn, M. G. (Michael G.)
Kang, Sang-Wook.
Langley Research Center.
Cornell Aeronautical Laboratory.

January 1973

"Prepared by Cornell Aeronautical Laboratory ... for Langley Research Center."Cover title.Bibliograp...

Low-speed aerodynamic characteristics of an airfoil optimized for maximum lift coefficient /

Bingham, Gene J.
Chen, Allen Wen-shin, 1945-
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 13.Mode of access: Internet

Water landing characteristics of a model of a winged reentry vehicle /

Abstract

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Water landing characteristics of a model of a winged reentry vehicle /

Abstract

Extracted data

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