Charts for determing potential minimum sonic-boom overpressures for supersonic cruise aircraft /

Investigation of a supersonic cruise fighter model flow field /

Reubush, David E.
Bare, E. Ann.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1985"--Cover.Includes bibliographical references (p. 8...

Aeroacoustic wind-tunnel tests of a light twin-boom general aviation airplane with free or shrouded-pusher propellers /

McLemore, H. Clyde.
Pegg, Robert J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"April 1980"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: In...

Supersonic flutter of panels loaded with inplane shear /

Sawyer, James Wayne, 1941-
Langely Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ...

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: ...

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

Supersonic cruise military aircraft research : an annotated bibliography /

Tuttle, Marie H.
Maddalon, Dal V.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Includes index."April 1980"--Cover."Langley Research Center."Mode of access: Internet

Subsonic maneuver capability of a supersonic cruise fighter wing concept /

Riebe, Gregory D.
Fox, Charles H.
Langley Research Center.

January 1987

Prepared at Langley Research Center."January 1987"--Cover.Includes bibliographical references (p. 10...

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...

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...

Supersonic wings with significant leading-edge thrust at cruise /

Robins, A. Warner.
Mack, Robert J.
Carlson, Harry W.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject Category 02."April 1980"--Cover."Langley Research Center."Includes bibliographical reference...

Supersonic aerodynamics of delta wings /

Wood, Richard M.
Langley Research Center.

January 1988

Prepared at Langley Research Center."March 1988"--Cover.Includes bibliographical references (p. 22-2...

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

Surface pressure data for a supersonic-cruise airplane configuration at mach numbers of 2.30, 2.96, and 3.30 /

Shrout, Barrett L.
Collins, Ida K.
Corlett, William A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

Subject category 02."May 1979"--Cover."Langley Research Center."Includes bibliographical references....

Lee-side flow over delta wings at supersonic speeds /

Miller, David S.
Wood, Richard M.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 150)....

Operating characteristics of the Langley Mach 7 Scramjet Test Facility /

Guy, Robert W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

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

Investigation of a supersonic cruise fighter model flow field /

Reubush, David E.
Bare, E. Ann.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1985"--Cover.Includes bibliographical references (p. 8...

Aeroacoustic wind-tunnel tests of a light twin-boom general aviation airplane with free or shrouded-pusher propellers /

McLemore, H. Clyde.
Pegg, Robert J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"April 1980"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: In...

Supersonic flutter of panels loaded with inplane shear /

Sawyer, James Wayne, 1941-
Langely Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ...

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: ...

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

Supersonic cruise military aircraft research : an annotated bibliography /

Tuttle, Marie H.
Maddalon, Dal V.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Includes index."April 1980"--Cover."Langley Research Center."Mode of access: Internet

Subsonic maneuver capability of a supersonic cruise fighter wing concept /

Riebe, Gregory D.
Fox, Charles H.
Langley Research Center.

January 1987

Prepared at Langley Research Center."January 1987"--Cover.Includes bibliographical references (p. 10...

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...

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...

Supersonic wings with significant leading-edge thrust at cruise /

Robins, A. Warner.
Mack, Robert J.
Carlson, Harry W.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject Category 02."April 1980"--Cover."Langley Research Center."Includes bibliographical reference...

Supersonic aerodynamics of delta wings /

Wood, Richard M.
Langley Research Center.

January 1988

Prepared at Langley Research Center."March 1988"--Cover.Includes bibliographical references (p. 22-2...

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

Surface pressure data for a supersonic-cruise airplane configuration at mach numbers of 2.30, 2.96, and 3.30 /

Shrout, Barrett L.
Collins, Ida K.
Corlett, William A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

Subject category 02."May 1979"--Cover."Langley Research Center."Includes bibliographical references....

Lee-side flow over delta wings at supersonic speeds /

Miller, David S.
Wood, Richard M.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 150)....

Operating characteristics of the Langley Mach 7 Scramjet Test Facility /

Guy, Robert W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

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

Investigation of a supersonic cruise fighter model flow field /

Reubush, David E.
Bare, E. Ann.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1985"--Cover.Includes bibliographical references (p. 8...

Aeroacoustic wind-tunnel tests of a light twin-boom general aviation airplane with free or shrouded-pusher propellers /

McLemore, H. Clyde.
Pegg, Robert J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"April 1980"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: In...

Supersonic flutter of panels loaded with inplane shear /

Sawyer, James Wayne, 1941-
Langely Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ...

Charts for determing potential minimum sonic-boom overpressures for supersonic cruise aircraft /

Abstract

Extracted data

Charts for determing potential minimum sonic-boom overpressures for supersonic cruise aircraft /

Abstract

Extracted data

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