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

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...

Drag of a supercritical body of revolution in free flight at transonic speeds and comparison with wind-tunnel data /

Usry, J. W.
Wallace, John W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."December 1971."Includes bibliographical references (p. 13).Mode...

Basic pressure measurements on a 0.0667-scale model of the North American X-15 research airplane at transonic speeds /

Osborne, Robert S.
Stafford, Virginia C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

"Langley Research Center, Langely Field, Va.""October 1960."Cover title.Includes bibliographical ref...

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

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

Ward, Vernon G.
Pearson, Merwin D.
Whitcomb, Charles F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"July 21, 1952."Includes bibliographical references (p. 21).Mode of access: Internet

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...

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 ...

Comparison of semispan data obtained in the Langley two-dimensional low-turbulence pressure tunnel and full-span data obtained in the Langley 19-foot pressure tunnel for a wing with a 40⁰ sweepback of the 0.27-chord line /

Cahill, Jones F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"April 22, 1949."Includes bibliographical references (p. 8).Mode of access: Internet

A transonic investigation of base pressures associated with shallow three-dimensional rearward-facing steps /

Kelly, Thomas C.
Langley Research Center.

Prepared at Langley Research Center."August 1965"--Cover.Includes bibliographical references (p. 11)...

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

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...

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

Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wing /

Keener, Earl R.
Flight Research Center (U.S.)

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 14-15).Mode of access: Internet

Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel /

Plentovich, Elizabeth B.
Gloss, Blair B.
Langley Research Center.

January 1986

Prepared at Langley Research Center."February 1986"--Cover.Includes bibliographical references (p. 8...

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...

Drag of a supercritical body of revolution in free flight at transonic speeds and comparison with wind-tunnel data /

Usry, J. W.
Wallace, John W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."December 1971."Includes bibliographical references (p. 13).Mode...

Basic pressure measurements on a 0.0667-scale model of the North American X-15 research airplane at transonic speeds /

Osborne, Robert S.
Stafford, Virginia C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

"Langley Research Center, Langely Field, Va.""October 1960."Cover title.Includes bibliographical ref...

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

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

Ward, Vernon G.
Pearson, Merwin D.
Whitcomb, Charles F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"July 21, 1952."Includes bibliographical references (p. 21).Mode of access: Internet

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...

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 ...

Comparison of semispan data obtained in the Langley two-dimensional low-turbulence pressure tunnel and full-span data obtained in the Langley 19-foot pressure tunnel for a wing with a 40⁰ sweepback of the 0.27-chord line /

Cahill, Jones F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"April 22, 1949."Includes bibliographical references (p. 8).Mode of access: Internet

A transonic investigation of base pressures associated with shallow three-dimensional rearward-facing steps /

Kelly, Thomas C.
Langley Research Center.

Prepared at Langley Research Center."August 1965"--Cover.Includes bibliographical references (p. 11)...

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

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...

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

Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wing /

Keener, Earl R.
Flight Research Center (U.S.)

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 14-15).Mode of access: Internet

Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel /

Plentovich, Elizabeth B.
Gloss, Blair B.
Langley Research Center.

January 1986

Prepared at Langley Research Center."February 1986"--Cover.Includes bibliographical references (p. 8...

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...

Drag of a supercritical body of revolution in free flight at transonic speeds and comparison with wind-tunnel data /

Usry, J. W.
Wallace, John W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."December 1971."Includes bibliographical references (p. 13).Mode...

Basic pressure measurements on a 0.0667-scale model of the North American X-15 research airplane at transonic speeds /

Osborne, Robert S.
Stafford, Virginia C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

"Langley Research Center, Langely Field, Va.""October 1960."Cover title.Includes bibliographical ref...

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

Abstract

Extracted data

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

Abstract

Extracted data

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