An experimental investigation of the transonic-flow-generation and shock-wave-reflection characteristics of a two-dimensional wind tunnel with 17-percent-open perforated walls /

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

A wind-tunnel investigation at a Mach number of 2.01 of the sonic-boom characteristics of three wing-body combinations differing in wing longitudinal location /

Morris, Odell A.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise.Includes bi...

A wind-tunnel investigation of the first-order vibratory stresses on a full-scale supersonic-type propeller operating in an asymmetric air flow /

Heath, Atwood R.
O'Neal, Robert L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"November 2, 1954."Includes bibliographical references (p. 14).Mode of access: Internet

A theoretical and experimental study of wind-tunnel-wall effects on oscillating air forces for two-dimensional subsonic compressible flow /

Runyan, Harry L.
Rainey, A. Gerald.
Woolston, Donald S.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"January 23, 1953."Includes bibliographical references (p. 24).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

Transonic wind-tunnel investigation of an unswept wing in combination with a systematic series of four bodies /

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

January 1953

"Janauary 6, 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

A method for the design of porous-wall wind tunnels /

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

January 1956

"January 20, 1956."Includes bibliographical references (p. 36).Mode of access: Internet

Investigations of the interaction of boundary layer and shock waves in transonic flow /

Liepmann, H. W. (Hans Wolfgang), 1914-2009, author.
Platt, Jospeh, author.
Goppert, Jean G., author.
California Institute of Technology, sponsor.
United States. Air Force. Air Matériel Command, issuing body.

Report prepared by the California Institute of Technology, Pasadena, California."9 February 1948."In...

Experimental investigation of flow through three highly loaded inlet guide vanes having different spanwise circulation gradients /

Beatty, Loren A.
Emery, James C.
Savage, Melvyn.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1952

"July 28, 1952."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

An experimental investigation of the effect of wind tunnel walls on the aerodynamic performance of a helicopter rotor /

Ganzer, Victor M.
Rae, William H.
University of Washington.

January 1960

"NASA TN D-415.""University of Washington.""May 1960."Cover title.Includes bibliographical reference...

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....

Experimental investigation at transonic speeds of pressure distributions over wedge and circular-arc airfoil sections and evaluation of perforated-wall interference /

Knechtel, Earl D. (Earl Dennis)
United States. National Aeronautics and Space Administration.

January 1959

Cover title.Includes bibliographical references (p. 20-21).Mode of access: Internet

Wind tunnel investigation of vortex flows on F/A-18 configuration at subsonic through transonic speeds /

Erickson, Gary E.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Includes bibliographical references (p. 20).Mode of access: Inte...

Transonic wind-tunnel investigation of the effects of aspect ratio, spanwise variations in section thickness ratio, and a body indentation on the aerodynamic characteristics of a 45©� sweptback wing-body combination /

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

January 1953

" January 27, 1953."Includes bibliographical references (p. 13).Mode of access: Internet

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

A wind-tunnel investigation at a Mach number of 2.01 of the sonic-boom characteristics of three wing-body combinations differing in wing longitudinal location /

Morris, Odell A.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise.Includes bi...

A wind-tunnel investigation of the first-order vibratory stresses on a full-scale supersonic-type propeller operating in an asymmetric air flow /

Heath, Atwood R.
O'Neal, Robert L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"November 2, 1954."Includes bibliographical references (p. 14).Mode of access: Internet

A theoretical and experimental study of wind-tunnel-wall effects on oscillating air forces for two-dimensional subsonic compressible flow /

Runyan, Harry L.
Rainey, A. Gerald.
Woolston, Donald S.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"January 23, 1953."Includes bibliographical references (p. 24).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

Transonic wind-tunnel investigation of an unswept wing in combination with a systematic series of four bodies /

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

January 1953

"Janauary 6, 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

A method for the design of porous-wall wind tunnels /

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

January 1956

"January 20, 1956."Includes bibliographical references (p. 36).Mode of access: Internet

Investigations of the interaction of boundary layer and shock waves in transonic flow /

Liepmann, H. W. (Hans Wolfgang), 1914-2009, author.
Platt, Jospeh, author.
Goppert, Jean G., author.
California Institute of Technology, sponsor.
United States. Air Force. Air Matériel Command, issuing body.

Report prepared by the California Institute of Technology, Pasadena, California."9 February 1948."In...

Experimental investigation of flow through three highly loaded inlet guide vanes having different spanwise circulation gradients /

Beatty, Loren A.
Emery, James C.
Savage, Melvyn.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1952

"July 28, 1952."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

An experimental investigation of the effect of wind tunnel walls on the aerodynamic performance of a helicopter rotor /

Ganzer, Victor M.
Rae, William H.
University of Washington.

January 1960

"NASA TN D-415.""University of Washington.""May 1960."Cover title.Includes bibliographical reference...

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....

Experimental investigation at transonic speeds of pressure distributions over wedge and circular-arc airfoil sections and evaluation of perforated-wall interference /

Knechtel, Earl D. (Earl Dennis)
United States. National Aeronautics and Space Administration.

January 1959

Cover title.Includes bibliographical references (p. 20-21).Mode of access: Internet

Wind tunnel investigation of vortex flows on F/A-18 configuration at subsonic through transonic speeds /

Erickson, Gary E.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Includes bibliographical references (p. 20).Mode of access: Inte...

Transonic wind-tunnel investigation of the effects of aspect ratio, spanwise variations in section thickness ratio, and a body indentation on the aerodynamic characteristics of a 45©� sweptback wing-body combination /

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

January 1953

" January 27, 1953."Includes bibliographical references (p. 13).Mode of access: Internet

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

A wind-tunnel investigation at a Mach number of 2.01 of the sonic-boom characteristics of three wing-body combinations differing in wing longitudinal location /

Morris, Odell A.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise.Includes bi...

A wind-tunnel investigation of the first-order vibratory stresses on a full-scale supersonic-type propeller operating in an asymmetric air flow /

Heath, Atwood R.
O'Neal, Robert L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"November 2, 1954."Includes bibliographical references (p. 14).Mode of access: Internet

An experimental investigation of the transonic-flow-generation and shock-wave-reflection characteristics of a two-dimensional wind tunnel with 17-percent-open perforated walls /

Abstract

Extracted data

An experimental investigation of the transonic-flow-generation and shock-wave-reflection characteristics of a two-dimensional wind tunnel with 17-percent-open perforated walls /

Abstract

Extracted data

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