Experimental aerodynamic performance characteristics of a rotor entry vehicle configuration : II. Transonic /

Investigation of the aerodynamic characteristics of two preliminary designs of Scout research vehicle at Mach numbers from 1.77 to 4.65 /

Keynton, Robert J.
Fichter, Ann B.
Langley Research Center.

Prepared at Langley Research Center."April 1961."Cover title.Includes bibliographical references (p....

An experimental investigation of an advanced turboprop installation on a swept wing at subsonic and transonic speeds /

Carlson, John R.
Pendergraft, Odis C.
Langley Research Center.

January 1987

"September 1987"--Cover.Prepared at Langley Research Center.Includes bibliographical references (p. ...

Transonic wind-tunnel investigation of the static aerodynamic characteristics of several configurations of the Blue Scout launch vehicle /

Kelly, Thomas C.
Keynton, Robert J.
Langley Research Center.

Prepared at Langley Research Center."September 1963"--Cover.Includes bibliographical references (p. ...

Experimental aerodynamic performance characteristics of a rotor entry vehicle configuration : III. Supersonic /

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.N71-16535.February 1971.Includes bibliographical references (p. 10)...

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 /

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

January 1968

Cover title."April 1968."Includes bibliographical references (p. 18).Mode of access: Internet

Experimental stability and control results at Mach 19 of an entry vehicle designed for an intermediate lift-drag ratio /

Johnston, Patrick J.
Witcofski, Robert D.
Langley Research Center.

Prepared at Langley Research Center."February 1968"--Cover.Includes bibliographical references (p. 1...

Experimental evaluation of inlet drag characteristics in the transonic mach number regime /

McVey, F. D., author.
Phillips, E. J., author.
Rejeske, J. V., author.
McDonnell Douglas Corporation. sponsor.
United States. Air Force. Systems Command. sponsor.
Air Force Aero Propulsion Laboratory (U.S.). issuing body.

"Final Report.""Project No. 3066, Task No. 306611.""November 1968."Includes bibliographical referenc...

Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers /

Dunham, Dana Morris.
Langley Research Center.

January 1987

Prepared at Langley Research Center."October 1987"--Cover.Includes bibliographical references (p. 57...

Experimental evaluation of inlet drag characteristics in the transonic mach number regime /

McVey, F. D., author.
Phillips, E. J., author.
Rejeske, J. V., author.
McDonnell Douglas Corporation. sponsor.
United States. Air Force. Systems Command. sponsor.
Air Force Aero Propulsion Laboratory (U.S.). issuing body.

"Project No. 3066, Task No. 306611.""Final Report, Supplement I.""November 1968."Includes bibliograp...

Dynamics of high-drag probe shapes at transonic speeds /

Sammonds, Robert I.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1971

Prepared at Ames Research Center."September 1971."N 71-33244.Includes bibliographical references (p....

Transonic performance of a Mach 2.65 auxiliary flow axisymmetric inlet /

Santman, Don M.
United States. National Aeronautics and Space Administration.
Ames Research Center.
Ellco Engineering, Inc.

January 1976

Issued Oct. 1976.Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

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

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...

Transonic flow analysis for rotors.

Chang, I-Chung.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1990

"June 1990."Cover title.Distributed to depository libraries in microfiche.Includes bibliographical r...

Investigation of the aerodynamic characteristics of two preliminary designs of Scout research vehicle at Mach numbers from 1.77 to 4.65 /

Keynton, Robert J.
Fichter, Ann B.
Langley Research Center.

Prepared at Langley Research Center."April 1961."Cover title.Includes bibliographical references (p....

An experimental investigation of an advanced turboprop installation on a swept wing at subsonic and transonic speeds /

Carlson, John R.
Pendergraft, Odis C.
Langley Research Center.

January 1987

"September 1987"--Cover.Prepared at Langley Research Center.Includes bibliographical references (p. ...

Transonic wind-tunnel investigation of the static aerodynamic characteristics of several configurations of the Blue Scout launch vehicle /

Kelly, Thomas C.
Keynton, Robert J.
Langley Research Center.

Prepared at Langley Research Center."September 1963"--Cover.Includes bibliographical references (p. ...

Experimental aerodynamic performance characteristics of a rotor entry vehicle configuration : III. Supersonic /

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.N71-16535.February 1971.Includes bibliographical references (p. 10)...

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 /

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

January 1968

Cover title."April 1968."Includes bibliographical references (p. 18).Mode of access: Internet

Experimental stability and control results at Mach 19 of an entry vehicle designed for an intermediate lift-drag ratio /

Johnston, Patrick J.
Witcofski, Robert D.
Langley Research Center.

Prepared at Langley Research Center."February 1968"--Cover.Includes bibliographical references (p. 1...

Experimental evaluation of inlet drag characteristics in the transonic mach number regime /

McVey, F. D., author.
Phillips, E. J., author.
Rejeske, J. V., author.
McDonnell Douglas Corporation. sponsor.
United States. Air Force. Systems Command. sponsor.
Air Force Aero Propulsion Laboratory (U.S.). issuing body.

"Final Report.""Project No. 3066, Task No. 306611.""November 1968."Includes bibliographical referenc...

Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers /

Dunham, Dana Morris.
Langley Research Center.

January 1987

Prepared at Langley Research Center."October 1987"--Cover.Includes bibliographical references (p. 57...

Experimental evaluation of inlet drag characteristics in the transonic mach number regime /

McVey, F. D., author.
Phillips, E. J., author.
Rejeske, J. V., author.
McDonnell Douglas Corporation. sponsor.
United States. Air Force. Systems Command. sponsor.
Air Force Aero Propulsion Laboratory (U.S.). issuing body.

"Project No. 3066, Task No. 306611.""Final Report, Supplement I.""November 1968."Includes bibliograp...

Dynamics of high-drag probe shapes at transonic speeds /

Sammonds, Robert I.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1971

Prepared at Ames Research Center."September 1971."N 71-33244.Includes bibliographical references (p....

Transonic performance of a Mach 2.65 auxiliary flow axisymmetric inlet /

Santman, Don M.
United States. National Aeronautics and Space Administration.
Ames Research Center.
Ellco Engineering, Inc.

January 1976

Issued Oct. 1976.Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

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

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...

Transonic flow analysis for rotors.

Chang, I-Chung.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1990

"June 1990."Cover title.Distributed to depository libraries in microfiche.Includes bibliographical r...

Investigation of the aerodynamic characteristics of two preliminary designs of Scout research vehicle at Mach numbers from 1.77 to 4.65 /

Keynton, Robert J.
Fichter, Ann B.
Langley Research Center.

Prepared at Langley Research Center."April 1961."Cover title.Includes bibliographical references (p....

An experimental investigation of an advanced turboprop installation on a swept wing at subsonic and transonic speeds /

Carlson, John R.
Pendergraft, Odis C.
Langley Research Center.

January 1987

"September 1987"--Cover.Prepared at Langley Research Center.Includes bibliographical references (p. ...

Transonic wind-tunnel investigation of the static aerodynamic characteristics of several configurations of the Blue Scout launch vehicle /

Kelly, Thomas C.
Keynton, Robert J.
Langley Research Center.

Prepared at Langley Research Center."September 1963"--Cover.Includes bibliographical references (p. ...

Experimental aerodynamic performance characteristics of a rotor entry vehicle configuration : II. Transonic /

Abstract

Extracted data

Experimental aerodynamic performance characteristics of a rotor entry vehicle configuration : II. Transonic /

Abstract

Extracted data

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