Investigation of sonic boom generated by thin, nonlifting, rectangular wings /

An investigation of transonic flow fields surrounding hot and cold sonic jets /

Lee, George.
Ames Research Center.

Prepared at Ames Research Center."April 1961."Cover title.Includes bibliographical references (p. 18...

Lateral-spread sonic-boom ground-pressure measurements from airplanes at altitudes to 75,000 feet and at Mach numbers to 2.0 /

Maglieri, Domenic J.
United States. National Aeronautics and Space Administration.
Langley Research Center.

"November 1963."Cover title.Includes bibliographical references.Mode of access: Internet

Simulated indoor sonic booms judged relative to noise from subsonic aircraft /

Kryter, Karl D.
Lukas, Jerome S., 1930-
Langley Research Center.
Stanford Research Institute.

January 1972

"Prepared by Stanford Research Institute ... for Langley Research Center."Cover title.Bibliography: ...

Some effects of mach number and geometry on sonic boom /

Hicks, R. M. (Raymond Morton), 1932-
Hunton, Lynn W.
Mendoza, Joel P.
Ames Research Center.

January 1967

Prepared at Ames Research Center.N67-38327.Cover title.Includes bibliographical references (p. 6).Mo...

Sonic boom propagation in a stratified atmosphere, with computer program /

Hayes, Wallace D.
Kulsrud, H. E.
Haefeli, Rudolph C.
United States. National Aeronautics and Space Administration.
Langley Research Center.
Aeronautical Research Associates of Princeton, Inc.

January 1969

"Prepared by Aeronautical Research Associates of Princeton, Inc. ... for Langley Research Center.""N...

Sonic boom in turbulence /

Horning, W. A.
United States. National Aeronautics and Space Administration.
Langley Research Center.
EG & G, inc.

January 1971

Prepared by EG & G, Inc. for Langley Research Center.N71-33283.Includes bibliographical references (...

An investigation of some aspects of the sonic boom by means of wind-tunnel measurements of pressures about several bodies at a mach number of 2.01 /

Carlson, Harry W.
United States. National Aeronautics and Space Administration.

Cover title."December 1959."Aerodynamics, fundamental; Bodies; Noise.Includes bibliographical refere...

Measurements of sonic booms generated by an airplane flying at Mach 3.5 and 4.8 /

Green, Karen S.
Putnam, Terrill W.
Flight Research Center (U.S.)

January 1974

Prepared at NASA Flight Research Center.Cover title.Includes bibliographical references (p. 8).Mode ...

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 study of the sonic-boom characteristics of a blunt body at a Mach number of 6 /

Ashby, George C.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Dec. 1980."Langley Research Center, Hampton, Virginia."Includes bibliographical references.Mode of a...

Investigation of flow-field development for a series of sonic-boom wind-tunnel models /

Runyan, Harry L.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Prepared at Langley Research Center.N71-20156.Issued Mar. 1971.Mode of access: Internet

Wind-tunnel investigation of the validity of a sonic-boom-minimization concept /

Mack, Robert J.
Darden, Christine M.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

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

An investigation of the influence of lift on sonic-boom intensity by means of wind-tunnel measurements of the pressure fields of several wing-body combinations at a mach number of 2.01 /

Carlson, Harry W.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircraft ...

Sonic-boom wave-front shapes and curvatures associated with maneuvering flight /

Barger, Raymond L.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject Category 02."December 1979"--Cover."Langley Research Center."Bibliography: p. 18.Mode of acc...

Flight test measurements and analysis of sonic boom phenomena near the shock wave extremity /

Haglund, George T. (George Thomas)
Kane, Edward J.
Langley Research Center.
Boeing Company.

January 1973

"Prepared by the Boeing Company ... for Langley Research Center."Cover title.Bibliography: p. 85-88....

An investigation of transonic flow fields surrounding hot and cold sonic jets /

Lee, George.
Ames Research Center.

Prepared at Ames Research Center."April 1961."Cover title.Includes bibliographical references (p. 18...

Lateral-spread sonic-boom ground-pressure measurements from airplanes at altitudes to 75,000 feet and at Mach numbers to 2.0 /

Maglieri, Domenic J.
United States. National Aeronautics and Space Administration.
Langley Research Center.

"November 1963."Cover title.Includes bibliographical references.Mode of access: Internet

Simulated indoor sonic booms judged relative to noise from subsonic aircraft /

Kryter, Karl D.
Lukas, Jerome S., 1930-
Langley Research Center.
Stanford Research Institute.

January 1972

"Prepared by Stanford Research Institute ... for Langley Research Center."Cover title.Bibliography: ...

Some effects of mach number and geometry on sonic boom /

Hicks, R. M. (Raymond Morton), 1932-
Hunton, Lynn W.
Mendoza, Joel P.
Ames Research Center.

January 1967

Prepared at Ames Research Center.N67-38327.Cover title.Includes bibliographical references (p. 6).Mo...

Sonic boom propagation in a stratified atmosphere, with computer program /

Hayes, Wallace D.
Kulsrud, H. E.
Haefeli, Rudolph C.
United States. National Aeronautics and Space Administration.
Langley Research Center.
Aeronautical Research Associates of Princeton, Inc.

January 1969

"Prepared by Aeronautical Research Associates of Princeton, Inc. ... for Langley Research Center.""N...

Sonic boom in turbulence /

Horning, W. A.
United States. National Aeronautics and Space Administration.
Langley Research Center.
EG & G, inc.

January 1971

Prepared by EG & G, Inc. for Langley Research Center.N71-33283.Includes bibliographical references (...

An investigation of some aspects of the sonic boom by means of wind-tunnel measurements of pressures about several bodies at a mach number of 2.01 /

Carlson, Harry W.
United States. National Aeronautics and Space Administration.

Cover title."December 1959."Aerodynamics, fundamental; Bodies; Noise.Includes bibliographical refere...

Measurements of sonic booms generated by an airplane flying at Mach 3.5 and 4.8 /

Green, Karen S.
Putnam, Terrill W.
Flight Research Center (U.S.)

January 1974

Prepared at NASA Flight Research Center.Cover title.Includes bibliographical references (p. 8).Mode ...

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 study of the sonic-boom characteristics of a blunt body at a Mach number of 6 /

Ashby, George C.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Dec. 1980."Langley Research Center, Hampton, Virginia."Includes bibliographical references.Mode of a...

Investigation of flow-field development for a series of sonic-boom wind-tunnel models /

Runyan, Harry L.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Prepared at Langley Research Center.N71-20156.Issued Mar. 1971.Mode of access: Internet

Wind-tunnel investigation of the validity of a sonic-boom-minimization concept /

Mack, Robert J.
Darden, Christine M.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

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

An investigation of the influence of lift on sonic-boom intensity by means of wind-tunnel measurements of the pressure fields of several wing-body combinations at a mach number of 2.01 /

Carlson, Harry W.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircraft ...

Sonic-boom wave-front shapes and curvatures associated with maneuvering flight /

Barger, Raymond L.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject Category 02."December 1979"--Cover."Langley Research Center."Bibliography: p. 18.Mode of acc...

Flight test measurements and analysis of sonic boom phenomena near the shock wave extremity /

Haglund, George T. (George Thomas)
Kane, Edward J.
Langley Research Center.
Boeing Company.

January 1973

"Prepared by the Boeing Company ... for Langley Research Center."Cover title.Bibliography: p. 85-88....

An investigation of transonic flow fields surrounding hot and cold sonic jets /

Lee, George.
Ames Research Center.

Prepared at Ames Research Center."April 1961."Cover title.Includes bibliographical references (p. 18...

Lateral-spread sonic-boom ground-pressure measurements from airplanes at altitudes to 75,000 feet and at Mach numbers to 2.0 /

Maglieri, Domenic J.
United States. National Aeronautics and Space Administration.
Langley Research Center.

"November 1963."Cover title.Includes bibliographical references.Mode of access: Internet

Simulated indoor sonic booms judged relative to noise from subsonic aircraft /

Kryter, Karl D.
Lukas, Jerome S., 1930-
Langley Research Center.
Stanford Research Institute.

January 1972

"Prepared by Stanford Research Institute ... for Langley Research Center."Cover title.Bibliography: ...

Investigation of sonic boom generated by thin, nonlifting, rectangular wings /

Abstract

Extracted data

Investigation of sonic boom generated by thin, nonlifting, rectangular wings /

Abstract

Extracted data

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