Flow-field measurements around a Mars lander model using hot-film anemometers under simulated Mars surface conditions /

Mach 6 flow field surveys beneath the forebody of an airbreatinng missile /

Johnston, Patrick J.
Hunt, James L. (James Larry), 1939-
Langley Research Center.

January 1986

Prepared at Langley Research Center."March 1986"--Cover.Includes bibliographical references (p. 151-...

Laser velocimeter systems analysis applied to a flow survey above a stalled wing /

Young, Warren H.
Hepner, Timothy E.
Meyers, James F.
Langley Directorate.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1977

Aug. 1977."Langley Directorate, U.S. Army Air Mobility R&D Laboratory, Hampton, Va.""Langley Resear...

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 ...

Saltation on Mars and expected lifetime of Viking 75 wind sensors /

Henry, Robert M.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 19).Mode of ...

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...

Development of an apparatus to measure thermophysical properties of wind tunnel heat transfer models /

Romanowski, Richard F.
Steinberg, Ira H.
Langley Research Center.
Grumman Aerospace Corporation.

January 1974

"Prepared by Grumman Aerospace Corporation ... for Langley Research Center."Cover title.Includes bib...

Flyby measurements of the profiles of water vapor, particulate matter, and carbon dioxide in the martian atmosphere /

Barrington, Alfred E.
Mannella, Gene G.
Caruso, A. J. (Anthony J.)
United States. National Aeronautics and Space Administration.
Electronics Research Center (U.S.)

Prepared at Electronics Research Center."August 1967"--Cover.Includes bibliographical references (p....

Radiation exposure for manned Mars surface missions /

Simonsen, Lisa C.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Includes bibliographical references (p. 9).Mode of access: Inter...

Mars gravitational field estimation error /

Compton, Harold R. (Harold Randolph), 1932-
Daniels, Edward F.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14).Mode of ...

An experimental investigation of base heating on typical Mars entry body shapes /

Zappa, O. L.
Reinecke, William G.
Langley Research Center.
Avco Corporation. Systems Division.

Prepared for Langley Research Center under contract no. NAS1-9368 by Avco Corporation Systems Divisi...

Flight test of an erectable spacecraft used for decelerator testing at simulated Mars entry conditions /

Henning, Allen B.
Lundstrom, Reginald R.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 22-24.Mode of access: Internet

Models of Mars atmosphere, 1967.

United States. National Aeronautics and Space Administration.

At head of title: NASA space vehicle design criteria: environment.Cover title.Bibliography: p. 15-16...

Measurements of flow rate and trajectory of aircraft tire-generated water spray /

Daugherty, Robert H.
Stubbs, Sandy M.
Langley Research Center.

January 1987

Prepared at Langley Research Center."July 1987"--Cover.Includes bibliographical references (p. 7).Mo...

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

The wedge hot-film anemometer in supersonic flow /

Seiner, John M.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1983

"Langley Research Center."Subject category 71."May 1983"--Cover.Mode of access: Internet

Mach 6 flow field surveys beneath the forebody of an airbreatinng missile /

Johnston, Patrick J.
Hunt, James L. (James Larry), 1939-
Langley Research Center.

January 1986

Prepared at Langley Research Center."March 1986"--Cover.Includes bibliographical references (p. 151-...

Laser velocimeter systems analysis applied to a flow survey above a stalled wing /

Young, Warren H.
Hepner, Timothy E.
Meyers, James F.
Langley Directorate.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1977

Aug. 1977."Langley Directorate, U.S. Army Air Mobility R&D Laboratory, Hampton, Va.""Langley Resear...

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 ...

Saltation on Mars and expected lifetime of Viking 75 wind sensors /

Henry, Robert M.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 19).Mode of ...

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...

Development of an apparatus to measure thermophysical properties of wind tunnel heat transfer models /

Romanowski, Richard F.
Steinberg, Ira H.
Langley Research Center.
Grumman Aerospace Corporation.

January 1974

"Prepared by Grumman Aerospace Corporation ... for Langley Research Center."Cover title.Includes bib...

Flyby measurements of the profiles of water vapor, particulate matter, and carbon dioxide in the martian atmosphere /

Barrington, Alfred E.
Mannella, Gene G.
Caruso, A. J. (Anthony J.)
United States. National Aeronautics and Space Administration.
Electronics Research Center (U.S.)

Prepared at Electronics Research Center."August 1967"--Cover.Includes bibliographical references (p....

Radiation exposure for manned Mars surface missions /

Simonsen, Lisa C.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Includes bibliographical references (p. 9).Mode of access: Inter...

Mars gravitational field estimation error /

Compton, Harold R. (Harold Randolph), 1932-
Daniels, Edward F.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14).Mode of ...

An experimental investigation of base heating on typical Mars entry body shapes /

Zappa, O. L.
Reinecke, William G.
Langley Research Center.
Avco Corporation. Systems Division.

Prepared for Langley Research Center under contract no. NAS1-9368 by Avco Corporation Systems Divisi...

Flight test of an erectable spacecraft used for decelerator testing at simulated Mars entry conditions /

Henning, Allen B.
Lundstrom, Reginald R.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 22-24.Mode of access: Internet

Models of Mars atmosphere, 1967.

United States. National Aeronautics and Space Administration.

At head of title: NASA space vehicle design criteria: environment.Cover title.Bibliography: p. 15-16...

Measurements of flow rate and trajectory of aircraft tire-generated water spray /

Daugherty, Robert H.
Stubbs, Sandy M.
Langley Research Center.

January 1987

Prepared at Langley Research Center."July 1987"--Cover.Includes bibliographical references (p. 7).Mo...

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

The wedge hot-film anemometer in supersonic flow /

Seiner, John M.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1983

"Langley Research Center."Subject category 71."May 1983"--Cover.Mode of access: Internet

Mach 6 flow field surveys beneath the forebody of an airbreatinng missile /

Johnston, Patrick J.
Hunt, James L. (James Larry), 1939-
Langley Research Center.

January 1986

Prepared at Langley Research Center."March 1986"--Cover.Includes bibliographical references (p. 151-...

Laser velocimeter systems analysis applied to a flow survey above a stalled wing /

Young, Warren H.
Hepner, Timothy E.
Meyers, James F.
Langley Directorate.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1977

Aug. 1977."Langley Directorate, U.S. Army Air Mobility R&D Laboratory, Hampton, Va.""Langley Resear...

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 ...

Flow-field measurements around a Mars lander model using hot-film anemometers under simulated Mars surface conditions /

Abstract

Extracted data

Flow-field measurements around a Mars lander model using hot-film anemometers under simulated Mars surface conditions /

Abstract

Extracted data

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