An analytical investigation of the aerodynamic and performance characteristics of an unpowered rotor entry vehicle /

Investigation of acceleration characteristics of a single-spool turbojet engine /

Oppenheimer, Frank L.
Pack, George J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "October 26, 1953."Title from cover.Includes bibliographical references: p. 13.Mode ...

Experimental investigation of the partial- admission performance characteristics of a single-stage Mach 2 supersonic turbine /

Moffitt, Thomas P.
Klag, Frederick W.
Langley Research Center.

January 1959

"September 1959."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Experimental aerodynamic performance characteristics of a rotor entry vehicle configuration : I. Subsonic /

Smith, Ronald C. (Ronald Carlton)
Levin, Alan D.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1971

Prepared at Ames Research Center.N71-16533.February 1971.Includes bibliographical references (p. 10)...

Critical-speed analysis of flexibly mounted rigid rotors /

Cavicchi, Richard H.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."June 1968."Includes bibliographical references (p. 50).Mode of access: Internet

Heat-transfer measurements on the rotor blade of a rotor entry vehicle model /

Smith, Ronald C.
Levin, Alan D.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 7).Mode of access: Internet

Hovering performance characteristics of a rotor with and without blade-pitch servo-control flaps /

Shivers, James P.
United States. National Aeronautics and Space Administration.

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

Analytical investigation of the dynamic behavior of a nonlifting manned reentry vehicle. /

Lichtenstein, Jacob H.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Includes bibliographical references.Mode of access: Internet

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

Stability analysis and minimum thrust vector control requirements of booster vehicles during atmospheric flight /

Borsody, Janos.
Teren, Fred.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 42).Mode of access: Internet

An approximate analytical method for studying atmosphere entry of vehicles with modulated aerodynamic forces /

Levy, Lionel L.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bib...

Flight investigation to determine the effect of longitudinal characteristics on low-speed instrument operation /

DiCarlo, Daniel J.
Sommer, Robert W.
Kelly, James R.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."March 1968."Includes bibliographical references (p. 17).Mode of access: Internet

Flight-test investigation of a model of an aerial vehicle supported by four unshrouded propellers /

Kirby, Robert H.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

Exploratory investigation of the aerodynamic characteristics of a biwing vehicle at Mach 20.3 /

Bernot, Peter T.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 4...

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

Force-test investigation of a model of an aerial vehicle supported by four unshrouded propellers /

Kirby, Robert H.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

Investigation of acceleration characteristics of a single-spool turbojet engine /

Oppenheimer, Frank L.
Pack, George J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "October 26, 1953."Title from cover.Includes bibliographical references: p. 13.Mode ...

Experimental investigation of the partial- admission performance characteristics of a single-stage Mach 2 supersonic turbine /

Moffitt, Thomas P.
Klag, Frederick W.
Langley Research Center.

January 1959

"September 1959."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Experimental aerodynamic performance characteristics of a rotor entry vehicle configuration : I. Subsonic /

Smith, Ronald C. (Ronald Carlton)
Levin, Alan D.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1971

Prepared at Ames Research Center.N71-16533.February 1971.Includes bibliographical references (p. 10)...

Critical-speed analysis of flexibly mounted rigid rotors /

Cavicchi, Richard H.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."June 1968."Includes bibliographical references (p. 50).Mode of access: Internet

Heat-transfer measurements on the rotor blade of a rotor entry vehicle model /

Smith, Ronald C.
Levin, Alan D.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 7).Mode of access: Internet

Hovering performance characteristics of a rotor with and without blade-pitch servo-control flaps /

Shivers, James P.
United States. National Aeronautics and Space Administration.

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

Analytical investigation of the dynamic behavior of a nonlifting manned reentry vehicle. /

Lichtenstein, Jacob H.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Includes bibliographical references.Mode of access: Internet

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

Stability analysis and minimum thrust vector control requirements of booster vehicles during atmospheric flight /

Borsody, Janos.
Teren, Fred.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 42).Mode of access: Internet

An approximate analytical method for studying atmosphere entry of vehicles with modulated aerodynamic forces /

Levy, Lionel L.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bib...

Flight investigation to determine the effect of longitudinal characteristics on low-speed instrument operation /

DiCarlo, Daniel J.
Sommer, Robert W.
Kelly, James R.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."March 1968."Includes bibliographical references (p. 17).Mode of access: Internet

Flight-test investigation of a model of an aerial vehicle supported by four unshrouded propellers /

Kirby, Robert H.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

Exploratory investigation of the aerodynamic characteristics of a biwing vehicle at Mach 20.3 /

Bernot, Peter T.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 4...

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

Force-test investigation of a model of an aerial vehicle supported by four unshrouded propellers /

Kirby, Robert H.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

Investigation of acceleration characteristics of a single-spool turbojet engine /

Oppenheimer, Frank L.
Pack, George J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "October 26, 1953."Title from cover.Includes bibliographical references: p. 13.Mode ...

Experimental investigation of the partial- admission performance characteristics of a single-stage Mach 2 supersonic turbine /

Moffitt, Thomas P.
Klag, Frederick W.
Langley Research Center.

January 1959

"September 1959."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Experimental aerodynamic performance characteristics of a rotor entry vehicle configuration : I. Subsonic /

Smith, Ronald C. (Ronald Carlton)
Levin, Alan D.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1971

Prepared at Ames Research Center.N71-16533.February 1971.Includes bibliographical references (p. 10)...

An analytical investigation of the aerodynamic and performance characteristics of an unpowered rotor entry vehicle /

Abstract

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An analytical investigation of the aerodynamic and performance characteristics of an unpowered rotor entry vehicle /

Abstract

Extracted data

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