Summary of rawinsonde measurements of temperatures, pressure heights, and winds above 50,000 feet along a flight-test range in the Southwestern United States /

Prediction of air temperature at a remote site from official weather station records /

Campbell, Ralph E. (Ralph Edmund), 1927-

Caption title.Includes bibliographical references (p. 4)Mode of access: Internet

Measurements of flow properties in the vicinity of three wing-fuselage combinations at Mach numbers of 1.61 and 2.01 /

Carlson, Harry W.
Langley Research Center.

January 1959

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

Summary of XB-70 airplane cockpit environmental data /

Irwin, Kirk S.
Andrews, William H.
United States. National Aeronautics and Space Administration.
Flight Research Center (U.S.)

Thermal, acoustical, and acceleration environments of XB-70 airplane crew compartment in airworthine...

Pressure measurements of the leading edge of a swept wing at Mach 2.2 /

Sorrells, Russell B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

Atmospheric pressure, density, temperature and wind variations between 50 and 200 km /

Justus, C. G. (Carl Gerald), 1939-
Woodrum, Arthur.
George C. Marshall Space Flight Center.
Georgia Institute of Technology.

January 1972

"Prepared by Georgia Institute of Technology ... for George C. Marshall Space Flight Center."Cover t...

Flight test of a pressuriztion system used to measure minor atmospheric constituents from an aircraft /

Reck, Gregory M., 1946-
Perkins, Porter J.
Briehl, Daniel.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode of...

High altitude gust acceleration environment as experienced by a supersonic airplane /

Ehernberger, L. J.
Love, Betty J.
Flight Research Center (U.S.)

January 1975

Prepared at NASA Flight Research Center.Cover title.Includes bibliographical references (p. 23-24).M...

Spectrographic temperature measurements in a carbon-arc-powered air jet /

Greenshields, David H.
Langley Research Center.

Prepared at Langley Research Center."December 1959."Cover title.Includes bibliographical references ...

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 (...

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

Experiments to study strain-gage load calibrations on a wing structure at elevated temperatures /

Monaghan, Richard C.
Fields, Roger A.
Flight Research Center (U.S.)

January 1973

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

Measurements of aerodynamic heating obtained during demonstration flight tests of the Douglas D-558-II airplane /

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

January 1952

"November 26, 1952."Includes bibliographical references (p. 8).Mode of access: Internet

Low-altitude wind measurements from wide-body jet transports /

Dunham, R. Earl.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"October 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Aerodynamic and landing measurements obtained during the first powered flight of the North American X-15 research airplane /

United States. National Aeronautics and Space Administration.
Flight Research Center (U.S.)

"January 1960."Cover title.Includes bibliographical references (p. 17).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

Prediction of air temperature at a remote site from official weather station records /

Campbell, Ralph E. (Ralph Edmund), 1927-

Caption title.Includes bibliographical references (p. 4)Mode of access: Internet

Measurements of flow properties in the vicinity of three wing-fuselage combinations at Mach numbers of 1.61 and 2.01 /

Carlson, Harry W.
Langley Research Center.

January 1959

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

Summary of XB-70 airplane cockpit environmental data /

Irwin, Kirk S.
Andrews, William H.
United States. National Aeronautics and Space Administration.
Flight Research Center (U.S.)

Thermal, acoustical, and acceleration environments of XB-70 airplane crew compartment in airworthine...

Pressure measurements of the leading edge of a swept wing at Mach 2.2 /

Sorrells, Russell B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

Atmospheric pressure, density, temperature and wind variations between 50 and 200 km /

Justus, C. G. (Carl Gerald), 1939-
Woodrum, Arthur.
George C. Marshall Space Flight Center.
Georgia Institute of Technology.

January 1972

"Prepared by Georgia Institute of Technology ... for George C. Marshall Space Flight Center."Cover t...

Flight test of a pressuriztion system used to measure minor atmospheric constituents from an aircraft /

Reck, Gregory M., 1946-
Perkins, Porter J.
Briehl, Daniel.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode of...

High altitude gust acceleration environment as experienced by a supersonic airplane /

Ehernberger, L. J.
Love, Betty J.
Flight Research Center (U.S.)

January 1975

Prepared at NASA Flight Research Center.Cover title.Includes bibliographical references (p. 23-24).M...

Spectrographic temperature measurements in a carbon-arc-powered air jet /

Greenshields, David H.
Langley Research Center.

Prepared at Langley Research Center."December 1959."Cover title.Includes bibliographical references ...

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 (...

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

Experiments to study strain-gage load calibrations on a wing structure at elevated temperatures /

Monaghan, Richard C.
Fields, Roger A.
Flight Research Center (U.S.)

January 1973

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

Measurements of aerodynamic heating obtained during demonstration flight tests of the Douglas D-558-II airplane /

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

January 1952

"November 26, 1952."Includes bibliographical references (p. 8).Mode of access: Internet

Low-altitude wind measurements from wide-body jet transports /

Dunham, R. Earl.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"October 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Aerodynamic and landing measurements obtained during the first powered flight of the North American X-15 research airplane /

United States. National Aeronautics and Space Administration.
Flight Research Center (U.S.)

"January 1960."Cover title.Includes bibliographical references (p. 17).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

Prediction of air temperature at a remote site from official weather station records /

Campbell, Ralph E. (Ralph Edmund), 1927-

Caption title.Includes bibliographical references (p. 4)Mode of access: Internet

Measurements of flow properties in the vicinity of three wing-fuselage combinations at Mach numbers of 1.61 and 2.01 /

Carlson, Harry W.
Langley Research Center.

January 1959

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

Summary of XB-70 airplane cockpit environmental data /

Irwin, Kirk S.
Andrews, William H.
United States. National Aeronautics and Space Administration.
Flight Research Center (U.S.)

Thermal, acoustical, and acceleration environments of XB-70 airplane crew compartment in airworthine...

Summary of rawinsonde measurements of temperatures, pressure heights, and winds above 50,000 feet along a flight-test range in the Southwestern United States /

Abstract

Extracted data

Summary of rawinsonde measurements of temperatures, pressure heights, and winds above 50,000 feet along a flight-test range in the Southwestern United States /

Abstract

Extracted data

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