Wind-tunnel investigation at mach numbers from 0.50 to 1.14 of the static aerodynamic characteristics of a model of a Project Mercury capsule /

A wind-tunnel investigation of the aerodynamic characteristics of a full-scale supersonic-type three-blade propeller at Mach numbers to 0.96 /

Evans, Albert J.
Liner, George.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"July 30, 1953."Includes bibliographical references (p. 14).Mode of access: Internet

Dynamic model tests at low subsonic speeds of Project Mercury capsule configurations with and without drogue parachutes /

Bowman, James S.
United States. National Aeronautics and Space Administration.

January 1961

"February 1961."Includes bibliographical references (p. 9).Mode of access: Internet

An investigation of some aspects of the sonic boom by means of wind-tunnel measurements of pressures about several bodies at a mach number of 2.01 /

Carlson, Harry W.
United States. National Aeronautics and Space Administration.

Cover title."December 1959."Aerodynamics, fundamental; Bodies; Noise.Includes bibliographical refere...

Wind-tunnel investigation of static aerodynamic characteristics of a 1/9-scale model of a Project Mercury capsule at mach numbers from 1.60 to 4.65 /

Shaw, David S.
Turner, Kenneth L.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Wind-tunnel investigation at Mach numbers from 0.60 to 1.20 of the static aerodynamic characteristics of a model of a possible nonlifting reentry capsule in combination with a rocket booster /

Pearson, Albin O.
Langley Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Static aerodynamic characteristics of a 1/9-scale model of the escape and exit configurations of the Project Mercury spacecraft at Mach numbers from 2.30 to 4.65 /

Fournier, Roger H.
Langley Research Center.

January 1962

"September 1962."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

A compilation of wind-tunnel heat-transfer measurements on the afterbody of the Project Mercury capsule reentry configuration /

Weston, Kenneth C.
Swanson, Joanna E.
United States. National Aeronautics and Space Administration. Space Task Group.

January 1961

"August 1961."Cover title.Includes bibliographical references (p. 13-14).Mode of access: Internet

Measurements of the surface flows, heat transfer, pressure distribution, and longitudinal stability of a mercury capsule model at Mach numbers of 6.9 and 9.6 /

Everhart, Philip E.
Bernot, Peter T.
Langley Research Center.

January 1961

"April 1961."Caption title.Includes bibliographical references (p. 13-14).Mode of access: Internet

Wind-tunnel investigation of thermal and pressure environments in the base of the Saturn S-IC booster from Mach 0.1 to 3.5 /

Wasko, Robert A.
United States. National Aeronautics and Space Administration.

Cover title."September 1966."Includes bibliographical references.Mode of access: Internet

Effects of canted forward faces on the static longitudinal stability characteristics of the escape and exit configurations of a project mercury capsule model at a mach number of 2.01 /

Harris, Roy V.
Robinson, Ross B.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 5).Mode of access: Internet

Wind-tunnel investigation of a small-scale model of an aerial vehicle supported by tilting ducted fans /

Smith, Charles C.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft; Stability and control.Includes bibliographical ref...

A wind-tunnel investigation at a Mach number of 2.01 of the sonic-boom characteristics of three wing-body combinations differing in wing longitudinal location /

Morris, Odell A.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise.Includes bi...

Full-scale wind-tunnel investigation of the aerodynamic characteristics of the X-24A lifting body aircraft /

Mort, Kenneth W.
Falarski, Michael D.
U.S. Army Aeronautical Research Laboratory.
Ames Research Center.
United States. National Aeronautics and Space Administration.

"August 1970."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Stability and drag characteristics at Mach numbers of 10 and 26 of a proposed slender atmospheric probe /

Malcolm, Gerald N.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."April 1967."Includes bibliographical references (p. 16).Mode of access: Internet

Full-scale wind-tunnel investigation of a flexible-wing manned test vehicle /

Johnson, Joseph L.
Hassell, James L.
United States. National Aeronautics and Space Administration.

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

A wind-tunnel investigation of the aerodynamic characteristics of a full-scale supersonic-type three-blade propeller at Mach numbers to 0.96 /

Evans, Albert J.
Liner, George.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"July 30, 1953."Includes bibliographical references (p. 14).Mode of access: Internet

Dynamic model tests at low subsonic speeds of Project Mercury capsule configurations with and without drogue parachutes /

Bowman, James S.
United States. National Aeronautics and Space Administration.

January 1961

"February 1961."Includes bibliographical references (p. 9).Mode of access: Internet

An investigation of some aspects of the sonic boom by means of wind-tunnel measurements of pressures about several bodies at a mach number of 2.01 /

Carlson, Harry W.
United States. National Aeronautics and Space Administration.

Cover title."December 1959."Aerodynamics, fundamental; Bodies; Noise.Includes bibliographical refere...

Wind-tunnel investigation of static aerodynamic characteristics of a 1/9-scale model of a Project Mercury capsule at mach numbers from 1.60 to 4.65 /

Shaw, David S.
Turner, Kenneth L.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Wind-tunnel investigation at Mach numbers from 0.60 to 1.20 of the static aerodynamic characteristics of a model of a possible nonlifting reentry capsule in combination with a rocket booster /

Pearson, Albin O.
Langley Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Static aerodynamic characteristics of a 1/9-scale model of the escape and exit configurations of the Project Mercury spacecraft at Mach numbers from 2.30 to 4.65 /

Fournier, Roger H.
Langley Research Center.

January 1962

"September 1962."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

A compilation of wind-tunnel heat-transfer measurements on the afterbody of the Project Mercury capsule reentry configuration /

Weston, Kenneth C.
Swanson, Joanna E.
United States. National Aeronautics and Space Administration. Space Task Group.

January 1961

"August 1961."Cover title.Includes bibliographical references (p. 13-14).Mode of access: Internet

Measurements of the surface flows, heat transfer, pressure distribution, and longitudinal stability of a mercury capsule model at Mach numbers of 6.9 and 9.6 /

Everhart, Philip E.
Bernot, Peter T.
Langley Research Center.

January 1961

"April 1961."Caption title.Includes bibliographical references (p. 13-14).Mode of access: Internet

Wind-tunnel investigation of thermal and pressure environments in the base of the Saturn S-IC booster from Mach 0.1 to 3.5 /

Wasko, Robert A.
United States. National Aeronautics and Space Administration.

Cover title."September 1966."Includes bibliographical references.Mode of access: Internet

Effects of canted forward faces on the static longitudinal stability characteristics of the escape and exit configurations of a project mercury capsule model at a mach number of 2.01 /

Harris, Roy V.
Robinson, Ross B.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 5).Mode of access: Internet

Wind-tunnel investigation of a small-scale model of an aerial vehicle supported by tilting ducted fans /

Smith, Charles C.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft; Stability and control.Includes bibliographical ref...

A wind-tunnel investigation at a Mach number of 2.01 of the sonic-boom characteristics of three wing-body combinations differing in wing longitudinal location /

Morris, Odell A.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise.Includes bi...

Full-scale wind-tunnel investigation of the aerodynamic characteristics of the X-24A lifting body aircraft /

Mort, Kenneth W.
Falarski, Michael D.
U.S. Army Aeronautical Research Laboratory.
Ames Research Center.
United States. National Aeronautics and Space Administration.

"August 1970."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Stability and drag characteristics at Mach numbers of 10 and 26 of a proposed slender atmospheric probe /

Malcolm, Gerald N.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."April 1967."Includes bibliographical references (p. 16).Mode of access: Internet

Full-scale wind-tunnel investigation of a flexible-wing manned test vehicle /

Johnson, Joseph L.
Hassell, James L.
United States. National Aeronautics and Space Administration.

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

A wind-tunnel investigation of the aerodynamic characteristics of a full-scale supersonic-type three-blade propeller at Mach numbers to 0.96 /

Evans, Albert J.
Liner, George.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"July 30, 1953."Includes bibliographical references (p. 14).Mode of access: Internet

Dynamic model tests at low subsonic speeds of Project Mercury capsule configurations with and without drogue parachutes /

Bowman, James S.
United States. National Aeronautics and Space Administration.

January 1961

"February 1961."Includes bibliographical references (p. 9).Mode of access: Internet

An investigation of some aspects of the sonic boom by means of wind-tunnel measurements of pressures about several bodies at a mach number of 2.01 /

Carlson, Harry W.
United States. National Aeronautics and Space Administration.

Cover title."December 1959."Aerodynamics, fundamental; Bodies; Noise.Includes bibliographical refere...

Wind-tunnel investigation at mach numbers from 0.50 to 1.14 of the static aerodynamic characteristics of a model of a Project Mercury capsule /

Abstract

Extracted data

Wind-tunnel investigation at mach numbers from 0.50 to 1.14 of the static aerodynamic characteristics of a model of a Project Mercury capsule /

Abstract

Extracted data

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