An experimental study of the validity of the heat-field concept for sonic-boom alleviation /

Loads induced on a flat plate at a Mach number of 4.5 with a sonic or supersonic jet exhausting normal to the surface /

Letko, William.
Langley Research Center.

Prepared at Langley Research Center."July 1963."Cover title.Includes bibliographical references (p. ...

Study of noise sources in a subsonic fan using measured blade pressures and acoustic theory /

Hanson, Donald B.
Langley Research Center.
United Technologies Corporation. Hamilton Standard Division.

"Prepared by Hamilton Standard ... for Langley Research Center.""August 1975."Cover title.Includes b...

A simulator study for the development and evaluation of operating procedures on a supersonic cruise research transport to minimize airport-community noise /

Grantham, William D.
Deal, Perry L.
Smith, Paul M., 1931-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Nov. 1980."Langley Research Center."Includes bibliographical references.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: ...

A study of the application of heat or force fields to the sonic-boom-minimization problem /

Miller, David S.
Carlson, Harry W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Sonic boom minimization by application of heat or force fields to airplane airflow.Prepared at Langl...

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....

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: ...

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...

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...

Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5 /

Rumsey, Charles B. (Charles Bertrand)
Hopko, Russell N.
Piland, Robert Owens.
Langley Research Center.

Prepared at Langley Research Center."January 1960."Cover title.Includes bibliographical references (...

Application of sonic-boom minimization concepts in supersonic transport design /

Carlson, Harry W.
Mack, Robert J.
Barger, Raymond L.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 42-44.Mode of access: Internet

A study for development of aerothermodynamic test model materials and fabrication technique /

Dean, W. G.
Connor, L. E.
Langley Research Center.
Lockheed Missiles and Space Company.

January 1972

"Prepared by Lockheed Missiles & Space Company ... for Langley Research Center."Cover title.Bibliogr...

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...

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 ...

A methodology for designing aircraft to low sonic boom constraints /

Mack, Robert J.
Needleman, Kathy E.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Includes bibliographical references (p. 6).Mode of access: Inter...

Loads induced on a flat plate at a Mach number of 4.5 with a sonic or supersonic jet exhausting normal to the surface /

Letko, William.
Langley Research Center.

Prepared at Langley Research Center."July 1963."Cover title.Includes bibliographical references (p. ...

Study of noise sources in a subsonic fan using measured blade pressures and acoustic theory /

Hanson, Donald B.
Langley Research Center.
United Technologies Corporation. Hamilton Standard Division.

"Prepared by Hamilton Standard ... for Langley Research Center.""August 1975."Cover title.Includes b...

A simulator study for the development and evaluation of operating procedures on a supersonic cruise research transport to minimize airport-community noise /

Grantham, William D.
Deal, Perry L.
Smith, Paul M., 1931-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Nov. 1980."Langley Research Center."Includes bibliographical references.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: ...

A study of the application of heat or force fields to the sonic-boom-minimization problem /

Miller, David S.
Carlson, Harry W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Sonic boom minimization by application of heat or force fields to airplane airflow.Prepared at Langl...

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....

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: ...

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...

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...

Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5 /

Rumsey, Charles B. (Charles Bertrand)
Hopko, Russell N.
Piland, Robert Owens.
Langley Research Center.

Prepared at Langley Research Center."January 1960."Cover title.Includes bibliographical references (...

Application of sonic-boom minimization concepts in supersonic transport design /

Carlson, Harry W.
Mack, Robert J.
Barger, Raymond L.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 42-44.Mode of access: Internet

A study for development of aerothermodynamic test model materials and fabrication technique /

Dean, W. G.
Connor, L. E.
Langley Research Center.
Lockheed Missiles and Space Company.

January 1972

"Prepared by Lockheed Missiles & Space Company ... for Langley Research Center."Cover title.Bibliogr...

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...

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 ...

A methodology for designing aircraft to low sonic boom constraints /

Mack, Robert J.
Needleman, Kathy E.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Includes bibliographical references (p. 6).Mode of access: Inter...

Loads induced on a flat plate at a Mach number of 4.5 with a sonic or supersonic jet exhausting normal to the surface /

Letko, William.
Langley Research Center.

Prepared at Langley Research Center."July 1963."Cover title.Includes bibliographical references (p. ...

Study of noise sources in a subsonic fan using measured blade pressures and acoustic theory /

Hanson, Donald B.
Langley Research Center.
United Technologies Corporation. Hamilton Standard Division.

"Prepared by Hamilton Standard ... for Langley Research Center.""August 1975."Cover title.Includes b...

A simulator study for the development and evaluation of operating procedures on a supersonic cruise research transport to minimize airport-community noise /

Grantham, William D.
Deal, Perry L.
Smith, Paul M., 1931-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Nov. 1980."Langley Research Center."Includes bibliographical references.Mode of access: Internet

An experimental study of the validity of the heat-field concept for sonic-boom alleviation /

Abstract

Extracted data

An experimental study of the validity of the heat-field concept for sonic-boom alleviation /

Abstract

Extracted data

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