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

Wind-tunnel investigation of the aerodynamic pressures on the Apollo command module configuration /

Moseley, William C.
Wells, B. J.
United States. National Aeronautics and Space Administration.
Manned Spacecraft Center (U.S.)

Wind tunnel study of aerodynamic pressures on Apollo command module configuration.Prepared at the Ma...

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

Aerodynamic loading characteristics of a 1/10-scale model of the three-stage Scout vehicle at Mach numbers 1.57 to 4.65 /

Jernell, Lloyd S.
Langley Research Center.

Prepared at Langley Research Center.Chiefly statistical tables."July 1963."Cover title.Includes bibl...

Transonic wind-tunnel investigation of the fin loads of a 1/8-scale model simulating the first stage of the Scout research vehicle /

Kelly, Thomas C.
Langley Research Center.

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

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....

Investigation of the static longitudinal aerodynamic characteristics of a 1/10-scale model of the Blue Scout Jr. at mach numbers from 0.40 to 1.03 /

Kelly, Thomas C.
Keynton, Robert J.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, missiles and space vehicles; Satellites; Stability and contro...

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

Dynamic and static wind-tunnel tests of a flow-direction vane /

Richardson, Norman R.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."April 1971."Cover title.Includes bibliographical references (p....

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

Wind-tunnel investigation of the flight characteristics of a canard general-aviation airplane configuration /

Satran, Dale R.
Langley Research Center.

January 1986

Prepared at Langley Research Center."October 1986"--Cover.Includes bibliographical references (p. 10...

Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration /

Alford, William J.
Handerson, William P.
Luoma, Arvo A.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Static stability characteristics of models of the Blue Scout and the Blue Scout, Jr., research vehicles at Mach numbers from 2.29 to 3.75 /

Jernell, Lloyd S.
Langley Research Center.

Prepared at Langley Research Center."July 1963."Cover title.Includes bibliographical references (p. ...

Low-speed wind-tunnel investigation of a series of twin-keel all-flexible parawings /

Naeseth, Roger L.
Langley Research Center.

January 1970

Prepared at Langley Research Center."October 1970."Cover title.Includes bibliographical references (...

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...

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

Wind-tunnel investigation of the aerodynamic pressures on the Apollo command module configuration /

Moseley, William C.
Wells, B. J.
United States. National Aeronautics and Space Administration.
Manned Spacecraft Center (U.S.)

Wind tunnel study of aerodynamic pressures on Apollo command module configuration.Prepared at the Ma...

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

Aerodynamic loading characteristics of a 1/10-scale model of the three-stage Scout vehicle at Mach numbers 1.57 to 4.65 /

Jernell, Lloyd S.
Langley Research Center.

Prepared at Langley Research Center.Chiefly statistical tables."July 1963."Cover title.Includes bibl...

Transonic wind-tunnel investigation of the fin loads of a 1/8-scale model simulating the first stage of the Scout research vehicle /

Kelly, Thomas C.
Langley Research Center.

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

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....

Investigation of the static longitudinal aerodynamic characteristics of a 1/10-scale model of the Blue Scout Jr. at mach numbers from 0.40 to 1.03 /

Kelly, Thomas C.
Keynton, Robert J.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, missiles and space vehicles; Satellites; Stability and contro...

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

Dynamic and static wind-tunnel tests of a flow-direction vane /

Richardson, Norman R.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."April 1971."Cover title.Includes bibliographical references (p....

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

Wind-tunnel investigation of the flight characteristics of a canard general-aviation airplane configuration /

Satran, Dale R.
Langley Research Center.

January 1986

Prepared at Langley Research Center."October 1986"--Cover.Includes bibliographical references (p. 10...

Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration /

Alford, William J.
Handerson, William P.
Luoma, Arvo A.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Static stability characteristics of models of the Blue Scout and the Blue Scout, Jr., research vehicles at Mach numbers from 2.29 to 3.75 /

Jernell, Lloyd S.
Langley Research Center.

Prepared at Langley Research Center."July 1963."Cover title.Includes bibliographical references (p. ...

Low-speed wind-tunnel investigation of a series of twin-keel all-flexible parawings /

Naeseth, Roger L.
Langley Research Center.

January 1970

Prepared at Langley Research Center."October 1970."Cover title.Includes bibliographical references (...

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...

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

Wind-tunnel investigation of the aerodynamic pressures on the Apollo command module configuration /

Moseley, William C.
Wells, B. J.
United States. National Aeronautics and Space Administration.
Manned Spacecraft Center (U.S.)

Wind tunnel study of aerodynamic pressures on Apollo command module configuration.Prepared at the Ma...

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

Aerodynamic loading characteristics of a 1/10-scale model of the three-stage Scout vehicle at Mach numbers 1.57 to 4.65 /

Jernell, Lloyd S.
Langley Research Center.

Prepared at Langley Research Center.Chiefly statistical tables."July 1963."Cover title.Includes bibl...

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

Abstract

Extracted data

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

Abstract

Extracted data

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