Air-flow and power characteristics of the Langley 16-foot transonic tunnel with slotted test section /

Studies of the use of Freon-12 as a testing medium in the Langley low-turbulence pressure tunnel /

von Doenhoff, Albert E.
Braslow, Albert L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1951

"December 5, 1951."Includes bibliographical references (p. 22).Mode of access: Internet

Laser velocimetry technique applied to the Langley 0.3-Meter transonic cryogenic tunnel /

Gartrell, Luther R.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"April 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: In...

Evaluation of flow quality in two large NASA wind tunnels at transonic speeds /

Harvey, Bill.
Owen, F. Kevin.
Stainback, P. Calvin.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Subject Category 34."December 1980"--Cover."Langley Research Center."Includes bibliographical refere...

Pressure measurements on a body of revolution in the Langley 16-foot transonic tunnel and a comparison with free-fall data /

Hallissy, Joseph M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"March 5, 1952."Includes bibliographical references (p. 9).Mode of access: Internet

An analysis of the pressure distribution measured on a body of revolution at transonic speeds in the slotted test section of the Langley 8-foot transonic tunnel /

Estabrooks, Bruce B.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"June 25, 1952."Includes bibliographical references (p. 23).Mode of access: Internet

Measurements of fluctuating pressures on the wing of a sweptback wind-body combination in the Langley 16-foot transonic tunnel /

Habel, Louis W.
Bowman, Donald R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"September 1, 1953."Includes bibliographical references (p. 11).Mode of access: Internet

Calibration of the Langley 16-foot transonic tunnel with test section air removal /

Corson, Blake W.
Igoe, William B.
Runckel, Jack F.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 38-39).Mode ...

Description and calibration of the Langley 6- by 19-inch transonic tunnel /

Ladson, Charles L.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 16-17.Mode of access: Internet

Improvement in the quality of flow visualization in the Langley 0.3-meter transonic cryogenic tunnel /

Snow, W. L.
Goad, William K.
Burner, Alpheus W.
Langley Research Center.

January 1986

Prepared at Lanagley Research Center."August 1986."Includes bibliographical references (p. 6).Mode o...

Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section /

McGhee, Robert J.
Beasley, William D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"November 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access:...

Dynamic measurement of total temperature, pressure, and velocity in the Langley 0.3-meter transonic cryogenic tunnel /

Johnson, Charles B.
Stainback, P. Calvin.
Langley Research Center.

January 1986

Prepared at Langley Research Center."May 1986"--Cover.Includes bibliographical references (p. 13).Mo...

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....

Description of recent changes in the Langley 6- by 28-inch transonic tunnel /

Sewall, William G.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 09."May 1981"--Cover."Langley Research Center."Includes bibliographical references....

Performance test of laser velocimeter system for the Langley 16-Foot Transonic Tunnel /

Meyers, James F.
United States. Army Aviation Systems Command. Aerostructures Directorate.
Langley Research Center.

January 1985

Prepared at Langley Research Center and Aerostructures Diectorate, USAARTA-AVSCOM."December 1985"--C...

Operating characteristics of the multiple critical venturi system and secondary calibration nozzles used for weight-flow measurements in the Langley 16-foot transonic tunnel /

Berrier, Bobby L.
Bangert, Linda S.
Leavitt, Laurence D.
Langley Research Center.

January 1985

Prepared at Langley Research Center."September 1985"--Cover.Includes bibliographical references (p. ...

Studies of the use of Freon-12 as a testing medium in the Langley low-turbulence pressure tunnel /

von Doenhoff, Albert E.
Braslow, Albert L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1951

"December 5, 1951."Includes bibliographical references (p. 22).Mode of access: Internet

Laser velocimetry technique applied to the Langley 0.3-Meter transonic cryogenic tunnel /

Gartrell, Luther R.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"April 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: In...

Evaluation of flow quality in two large NASA wind tunnels at transonic speeds /

Harvey, Bill.
Owen, F. Kevin.
Stainback, P. Calvin.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Subject Category 34."December 1980"--Cover."Langley Research Center."Includes bibliographical refere...

Pressure measurements on a body of revolution in the Langley 16-foot transonic tunnel and a comparison with free-fall data /

Hallissy, Joseph M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"March 5, 1952."Includes bibliographical references (p. 9).Mode of access: Internet

An analysis of the pressure distribution measured on a body of revolution at transonic speeds in the slotted test section of the Langley 8-foot transonic tunnel /

Estabrooks, Bruce B.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"June 25, 1952."Includes bibliographical references (p. 23).Mode of access: Internet

Measurements of fluctuating pressures on the wing of a sweptback wind-body combination in the Langley 16-foot transonic tunnel /

Habel, Louis W.
Bowman, Donald R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"September 1, 1953."Includes bibliographical references (p. 11).Mode of access: Internet

Calibration of the Langley 16-foot transonic tunnel with test section air removal /

Corson, Blake W.
Igoe, William B.
Runckel, Jack F.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 38-39).Mode ...

Description and calibration of the Langley 6- by 19-inch transonic tunnel /

Ladson, Charles L.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 16-17.Mode of access: Internet

Improvement in the quality of flow visualization in the Langley 0.3-meter transonic cryogenic tunnel /

Snow, W. L.
Goad, William K.
Burner, Alpheus W.
Langley Research Center.

January 1986

Prepared at Lanagley Research Center."August 1986."Includes bibliographical references (p. 6).Mode o...

Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section /

McGhee, Robert J.
Beasley, William D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"November 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access:...

Dynamic measurement of total temperature, pressure, and velocity in the Langley 0.3-meter transonic cryogenic tunnel /

Johnson, Charles B.
Stainback, P. Calvin.
Langley Research Center.

January 1986

Prepared at Langley Research Center."May 1986"--Cover.Includes bibliographical references (p. 13).Mo...

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....

Description of recent changes in the Langley 6- by 28-inch transonic tunnel /

Sewall, William G.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 09."May 1981"--Cover."Langley Research Center."Includes bibliographical references....

Performance test of laser velocimeter system for the Langley 16-Foot Transonic Tunnel /

Meyers, James F.
United States. Army Aviation Systems Command. Aerostructures Directorate.
Langley Research Center.

January 1985

Prepared at Langley Research Center and Aerostructures Diectorate, USAARTA-AVSCOM."December 1985"--C...

Operating characteristics of the multiple critical venturi system and secondary calibration nozzles used for weight-flow measurements in the Langley 16-foot transonic tunnel /

Berrier, Bobby L.
Bangert, Linda S.
Leavitt, Laurence D.
Langley Research Center.

January 1985

Prepared at Langley Research Center."September 1985"--Cover.Includes bibliographical references (p. ...

Studies of the use of Freon-12 as a testing medium in the Langley low-turbulence pressure tunnel /

von Doenhoff, Albert E.
Braslow, Albert L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1951

"December 5, 1951."Includes bibliographical references (p. 22).Mode of access: Internet

Laser velocimetry technique applied to the Langley 0.3-Meter transonic cryogenic tunnel /

Gartrell, Luther R.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"April 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: In...

Evaluation of flow quality in two large NASA wind tunnels at transonic speeds /

Harvey, Bill.
Owen, F. Kevin.
Stainback, P. Calvin.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Subject Category 34."December 1980"--Cover."Langley Research Center."Includes bibliographical refere...

Air-flow and power characteristics of the Langley 16-foot transonic tunnel with slotted test section /

Abstract

Extracted data

Air-flow and power characteristics of the Langley 16-foot transonic tunnel with slotted test section /

Abstract

Extracted data

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