Aerodynamic characteristics of a series of twin-inlet air-breathing missile configurations /

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...

Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at mach 1.60, 2.36, and 3.70 /

Lamb, Milton.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 02."August 1979"--Cover.v. 1. Trapezoidal tail -- v. 2. Clipped delta tail -- v. 3....

Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds /

Leavitt, Laurence D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"October 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: ...

Aerodynamic characteristics of a series of twin-inlet air-breathing missile configurations. 2: Two-dimensional inlets at supersonic speeds

Hayes, C.

March 1983

A series of air-breathing missile configurations was investigated to provide a data base for the des...

Aerodynamic characteristics of a Sparrow III missile model in the flow field of a generalized parent body at Mach 2.86 /

Stallings, Robert L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1981

"February 1984"--Cover.Includes bibliographical references.Mode of access: Internet

Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets /

Trefny, Charles J.
Wasserbauer, Joseph W.
Lewis Research Center.

January 1986

Prepared at Lewis Research Center."February 1986"--Cover.Includes bibliographical references (p. 10)...

Aeropropulsive characteristics of twin single-expansion-ramp vectoring nozzles installed with forward-swept wings and canards /

Mason, Mary L.
Capone, Francis J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"March 1983"--Cover.Includes bibliographical references.Mode of access: Internet

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

Development of a three-dimensional supersonic inlet flow analysis /

Buggeln, R. C.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"January 1980"--Cover.Includes bibliographical references.Mode of access: Internet

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

Aeropropulsive characteristics of twin nonaxisymmetric vectoring nozzles installed with forward swept and aft-swept wings /

Capone, Francis J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 02."March 1981"--Cover.Includes bibliographical references.Mode of access: Internet

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...

Aerodynamic characteristics of a series of single-inlet air-breathing missile configurations

Hayes, C.

March 1983

A series of air-breathing missile configurations was investigated to provide a data base for the des...

Aerodynamic characteristics in pitch of a 1/7-scale model of a two- and three-stage rocket configuration at Mach numbers of 0.4 to 4.63 /

Hinson, William F.
Fournier, Roger H.
Langhans, Richard A.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Aerodynamic characteristics in pitch of scale model of two and three stage rocket configuration at M...

Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a mach number of 2.01 /

Foster, Gerald V.
Langley Research Center.

January 1959

"November 1959"--Cover.Caption title.Includes bibliographical references (p. 6).Mode of access: Inte...

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...

Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at mach 1.60, 2.36, and 3.70 /

Lamb, Milton.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 02."August 1979"--Cover.v. 1. Trapezoidal tail -- v. 2. Clipped delta tail -- v. 3....

Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds /

Leavitt, Laurence D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"October 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: ...

Aerodynamic characteristics of a series of twin-inlet air-breathing missile configurations. 2: Two-dimensional inlets at supersonic speeds

Hayes, C.

March 1983

A series of air-breathing missile configurations was investigated to provide a data base for the des...

Aerodynamic characteristics of a Sparrow III missile model in the flow field of a generalized parent body at Mach 2.86 /

Stallings, Robert L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1981

"February 1984"--Cover.Includes bibliographical references.Mode of access: Internet

Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets /

Trefny, Charles J.
Wasserbauer, Joseph W.
Lewis Research Center.

January 1986

Prepared at Lewis Research Center."February 1986"--Cover.Includes bibliographical references (p. 10)...

Aeropropulsive characteristics of twin single-expansion-ramp vectoring nozzles installed with forward-swept wings and canards /

Mason, Mary L.
Capone, Francis J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"March 1983"--Cover.Includes bibliographical references.Mode of access: Internet

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

Development of a three-dimensional supersonic inlet flow analysis /

Buggeln, R. C.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"January 1980"--Cover.Includes bibliographical references.Mode of access: Internet

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

Aeropropulsive characteristics of twin nonaxisymmetric vectoring nozzles installed with forward swept and aft-swept wings /

Capone, Francis J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 02."March 1981"--Cover.Includes bibliographical references.Mode of access: Internet

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...

Aerodynamic characteristics of a series of single-inlet air-breathing missile configurations

Hayes, C.

March 1983

A series of air-breathing missile configurations was investigated to provide a data base for the des...

Aerodynamic characteristics in pitch of a 1/7-scale model of a two- and three-stage rocket configuration at Mach numbers of 0.4 to 4.63 /

Hinson, William F.
Fournier, Roger H.
Langhans, Richard A.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Aerodynamic characteristics in pitch of scale model of two and three stage rocket configuration at M...

Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a mach number of 2.01 /

Foster, Gerald V.
Langley Research Center.

January 1959

"November 1959"--Cover.Caption title.Includes bibliographical references (p. 6).Mode of access: Inte...

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...

Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at mach 1.60, 2.36, and 3.70 /

Lamb, Milton.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 02."August 1979"--Cover.v. 1. Trapezoidal tail -- v. 2. Clipped delta tail -- v. 3....

Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds /

Leavitt, Laurence D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"October 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: ...

Aerodynamic characteristics of a series of twin-inlet air-breathing missile configurations /

Abstract

Extracted data

Aerodynamic characteristics of a series of twin-inlet air-breathing missile configurations /

Abstract

Extracted data

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