The development of an 8-inch by 8-inch slotted tunnel from mach numbers up to 1.28 /

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 /

Pearson, Albin O.
United States. National Aeronautics and Space Administration.

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

Experimental study of the ionization of low-density gas flows by induced discharges /

Barger, R. L.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Major NASA subject terms:Includes bibliographical references.Mode of ac...

Wind-tunnel tests of a series of 18-foot-diameter parachutes with extendable flaps /

Gamse, Berl.
Yaggy, Paul F.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bibl...

Investigation of an axisymmetric internal compression inlet at a mach number of about 3.8 /

Lundell, John H.
Anderson, Lewis A.
Scherrer, Richard.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Major NASA subject terms: Aircraft; Propulsion system elements; Propulsion s...

Wind-tunnel investigation of a balloon as a towed deceleration at mach numbers from 1.47 to 2.50 /

McShera, John T.
Keyes, J. Wayne.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Aircr...

Boundary-layer transition on a group of blunt nose shapes at a mach number of 2.20 /

Jackson, Mary W.
Czatnecki, K. R.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Major NASA subject terms: Aerodynamics, aircraft; Aerodynamics, missiles and...

The development of an 8-inch by 8-inch slotted tunnel for Mach numbers up to 1.28 /

Little, B. H.
Cubbage, James M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"May 10, 1955."Includes bibliographical references (p. 26-27).Mode of access: Internet

Aerodynamic characteristics at a mach number of 3.10 of several fourth-stage shapes of the scout research vehicle /

Jaquet, Byron M.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Missile...

Design and calibration of an arc-heated, hypersonic, low-density wind tunnel

Weitmann, Ruth N.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Chemistry, p...

Problems involved in an emergency method of guiding a gliding vehicle from high altitudes to a high key position /

Jewel, Joseph W.
United States. National Aeronautics and Space Administration.

Cover title." August 1960."Major NASA subject terms:Includes bibliographical references.Mode of acce...

A transonic investigation of changing indentation design Mach number on the aerodynamic characteristics of a 45 degree sweptback-wing-body combination designed for high performance /

Loving, Donald L.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Major NASA subject terms:Aerodynamics, aircraft; Aircraft; Stability and ...

Description of a 2-foot hypersonic facility at the Langley Research Center /

Stokes, George M.
Langley Research Center.

Prepared at Langley Research Center."September 1961."Cover title.Includes bibliographical references...

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

Local aerodynamic heat transfer and boundary-layer transition on roughened sphere-ellipsoid bodies at mach number 3.0/

Deveikis, William D.
Walker, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Fluid...

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 0.50 to 1.14 of the static aerodynamic characteristics of a model of a Project Mercury capsule /

Pearson, Albin O.
United States. National Aeronautics and Space Administration.

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

Experimental study of the ionization of low-density gas flows by induced discharges /

Barger, R. L.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Major NASA subject terms:Includes bibliographical references.Mode of ac...

Wind-tunnel tests of a series of 18-foot-diameter parachutes with extendable flaps /

Gamse, Berl.
Yaggy, Paul F.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bibl...

Investigation of an axisymmetric internal compression inlet at a mach number of about 3.8 /

Lundell, John H.
Anderson, Lewis A.
Scherrer, Richard.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Major NASA subject terms: Aircraft; Propulsion system elements; Propulsion s...

Wind-tunnel investigation of a balloon as a towed deceleration at mach numbers from 1.47 to 2.50 /

McShera, John T.
Keyes, J. Wayne.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Aircr...

Boundary-layer transition on a group of blunt nose shapes at a mach number of 2.20 /

Jackson, Mary W.
Czatnecki, K. R.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Major NASA subject terms: Aerodynamics, aircraft; Aerodynamics, missiles and...

The development of an 8-inch by 8-inch slotted tunnel for Mach numbers up to 1.28 /

Little, B. H.
Cubbage, James M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"May 10, 1955."Includes bibliographical references (p. 26-27).Mode of access: Internet

Aerodynamic characteristics at a mach number of 3.10 of several fourth-stage shapes of the scout research vehicle /

Jaquet, Byron M.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Missile...

Design and calibration of an arc-heated, hypersonic, low-density wind tunnel

Weitmann, Ruth N.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Chemistry, p...

Problems involved in an emergency method of guiding a gliding vehicle from high altitudes to a high key position /

Jewel, Joseph W.
United States. National Aeronautics and Space Administration.

Cover title." August 1960."Major NASA subject terms:Includes bibliographical references.Mode of acce...

A transonic investigation of changing indentation design Mach number on the aerodynamic characteristics of a 45 degree sweptback-wing-body combination designed for high performance /

Loving, Donald L.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Major NASA subject terms:Aerodynamics, aircraft; Aircraft; Stability and ...

Description of a 2-foot hypersonic facility at the Langley Research Center /

Stokes, George M.
Langley Research Center.

Prepared at Langley Research Center."September 1961."Cover title.Includes bibliographical references...

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

Local aerodynamic heat transfer and boundary-layer transition on roughened sphere-ellipsoid bodies at mach number 3.0/

Deveikis, William D.
Walker, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Fluid...

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 0.50 to 1.14 of the static aerodynamic characteristics of a model of a Project Mercury capsule /

Pearson, Albin O.
United States. National Aeronautics and Space Administration.

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

Experimental study of the ionization of low-density gas flows by induced discharges /

Barger, R. L.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Major NASA subject terms:Includes bibliographical references.Mode of ac...

Wind-tunnel tests of a series of 18-foot-diameter parachutes with extendable flaps /

Gamse, Berl.
Yaggy, Paul F.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bibl...

The development of an 8-inch by 8-inch slotted tunnel from mach numbers up to 1.28 /

Abstract

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The development of an 8-inch by 8-inch slotted tunnel from mach numbers up to 1.28 /

Abstract

Extracted data

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