Flight evaluation of a pneumatic system for unsteady pressure measurements using conventional sensors /

Unsteady aerodynamics for advanced configurations.

Li, T. C., author.
United States. Air Force. Systems Command. issuing body.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
North American Aviation. Space and Information Systems Division. sponsor.

Includes bibliograpical references (page 42).Air Force Contract No.Mode of access: Internet

Flight investigation of manual and automatic VTOL decelerating instrument approaches and landings /

Kelly, James R.
Langley Research Center.

January 1974

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

Pressure distribution on a vectored-thrust V/STOL fighter in the transition-speed range /

Mineck, Raymond E.
Margason, Richard J. (Richard John), 1936-
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Bibliography: p. 11.Mode of access: Internet

A Preliminary investigation of the use of throttles for emergency flight control /

Burcham, Frank W.
Dryden Flight Research Facility.

January 1991

Prepared at Dryden Flight Research Facility.Bibliography: p. 9.Mode of access: Internet

Development of an integrated aeroservoelastic analysis program and correlation with test data /

Gupta, Kajal K.
Voelker, L. S.
Brenner, M. J.
Dryden Flight Research Facility.

January 1991

Prepared at the Dryden Flight Research Facility.Bibliography: p. 39.Mode of access: Internet

Propulsion system/flight control integration and optimization : flight evaluation and technology transition /

Burcham, Frank W.
Myers, Lawrence P.
Gilyard, Glenn B.
Dryden Flight Research Facility.

January 1990

Prepared at Dryden Flight Research Facility.Bibliography: p. 9-10.Mode of access: Internet

An in-flight technique for wind measurement in support of the space shuttle program /

Bjarke, Lisa J.
Ehernberger, L. J.
Dryden Flight Research Facility.

January 1989

Research performed at Dryden Flight Research Facility.Bibliography: p. 6.Mode of access: Internet

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...

Measurements of pressure on the tail and aft fuselage of an airplabne model during rotary motions at spin attitudes /

Bowman, James S. (James Scarboro), 1924-
Martin, Colin A.
Hultberg, Randy S.
Langley Research Center.

January 1989

Research performed at Langley Research Center.Bibliography: p. 53.Mode of access: Internet

Flight control system design factors for applying automated testing techniques /

Sitz, Joel R.
Vernon, Todd H.
Dryden Flight Research Facility.

January 1990

Prepared at Dryden Flight Research Facility, Ames Research Center.Bibliography: p. 7-8.Mode of acces...

Measurements of surface-pressure fluctuations on the XB-70 airplane at local Mach numbers up to 2.45 /

Lewis, Thomas L.
Hanly, Richard D.
Dods, Jules B.
Flight Research Center (U.S.)

January 1973

Prepared at the NASA Flight Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

Measurement effects on the calculation of in-flight thrust for an F404 turbofan engine /

Conners, Timothy E.
Dryden Flight Research Facility.

January 1989

Research performed at Dryden Flight Research Facility.Includes bibliographical references (p. 8).Mod...

Subsonic tests of an all-flush-pressure-orifice air data system /

Larson, Terry J.
Siemers, Paul M.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.
Hugh L. Dryden Flight Research Center.

January 1981

"June 1981"--Cover."Langley Research Center.""Dryden Flight Research Center."Includes bibliographica...

Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode /

Lance, Michael B.
Stroub, Robert H.
Sung, Daniel Y.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Bibliography: p. 24.Mode of access: Internet

Flight measurements of surface pressures on a flexible supercritical research wing /

Eckstrom, Clinton V.
Langley Research Center.

January 1985

Prepared at Langley Research Center."December 1985"--Cover.Includes bibliographical references (p. 1...

Unsteady aerodynamics for advanced configurations.

Li, T. C., author.
United States. Air Force. Systems Command. issuing body.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
North American Aviation. Space and Information Systems Division. sponsor.

Includes bibliograpical references (page 42).Air Force Contract No.Mode of access: Internet

Flight investigation of manual and automatic VTOL decelerating instrument approaches and landings /

Kelly, James R.
Langley Research Center.

January 1974

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

Pressure distribution on a vectored-thrust V/STOL fighter in the transition-speed range /

Mineck, Raymond E.
Margason, Richard J. (Richard John), 1936-
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Bibliography: p. 11.Mode of access: Internet

A Preliminary investigation of the use of throttles for emergency flight control /

Burcham, Frank W.
Dryden Flight Research Facility.

January 1991

Prepared at Dryden Flight Research Facility.Bibliography: p. 9.Mode of access: Internet

Development of an integrated aeroservoelastic analysis program and correlation with test data /

Gupta, Kajal K.
Voelker, L. S.
Brenner, M. J.
Dryden Flight Research Facility.

January 1991

Prepared at the Dryden Flight Research Facility.Bibliography: p. 39.Mode of access: Internet

Propulsion system/flight control integration and optimization : flight evaluation and technology transition /

Burcham, Frank W.
Myers, Lawrence P.
Gilyard, Glenn B.
Dryden Flight Research Facility.

January 1990

Prepared at Dryden Flight Research Facility.Bibliography: p. 9-10.Mode of access: Internet

An in-flight technique for wind measurement in support of the space shuttle program /

Bjarke, Lisa J.
Ehernberger, L. J.
Dryden Flight Research Facility.

January 1989

Research performed at Dryden Flight Research Facility.Bibliography: p. 6.Mode of access: Internet

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...

Measurements of pressure on the tail and aft fuselage of an airplabne model during rotary motions at spin attitudes /

Bowman, James S. (James Scarboro), 1924-
Martin, Colin A.
Hultberg, Randy S.
Langley Research Center.

January 1989

Research performed at Langley Research Center.Bibliography: p. 53.Mode of access: Internet

Flight control system design factors for applying automated testing techniques /

Sitz, Joel R.
Vernon, Todd H.
Dryden Flight Research Facility.

January 1990

Prepared at Dryden Flight Research Facility, Ames Research Center.Bibliography: p. 7-8.Mode of acces...

Measurements of surface-pressure fluctuations on the XB-70 airplane at local Mach numbers up to 2.45 /

Lewis, Thomas L.
Hanly, Richard D.
Dods, Jules B.
Flight Research Center (U.S.)

January 1973

Prepared at the NASA Flight Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

Measurement effects on the calculation of in-flight thrust for an F404 turbofan engine /

Conners, Timothy E.
Dryden Flight Research Facility.

January 1989

Research performed at Dryden Flight Research Facility.Includes bibliographical references (p. 8).Mod...

Subsonic tests of an all-flush-pressure-orifice air data system /

Larson, Terry J.
Siemers, Paul M.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.
Hugh L. Dryden Flight Research Center.

January 1981

"June 1981"--Cover."Langley Research Center.""Dryden Flight Research Center."Includes bibliographica...

Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode /

Lance, Michael B.
Stroub, Robert H.
Sung, Daniel Y.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Bibliography: p. 24.Mode of access: Internet

Flight measurements of surface pressures on a flexible supercritical research wing /

Eckstrom, Clinton V.
Langley Research Center.

January 1985

Prepared at Langley Research Center."December 1985"--Cover.Includes bibliographical references (p. 1...

Unsteady aerodynamics for advanced configurations.

Li, T. C., author.
United States. Air Force. Systems Command. issuing body.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
North American Aviation. Space and Information Systems Division. sponsor.

Includes bibliograpical references (page 42).Air Force Contract No.Mode of access: Internet

Flight investigation of manual and automatic VTOL decelerating instrument approaches and landings /

Kelly, James R.
Langley Research Center.

January 1974

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

Pressure distribution on a vectored-thrust V/STOL fighter in the transition-speed range /

Mineck, Raymond E.
Margason, Richard J. (Richard John), 1936-
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Bibliography: p. 11.Mode of access: Internet

Flight evaluation of a pneumatic system for unsteady pressure measurements using conventional sensors /

Abstract

Extracted data

Flight evaluation of a pneumatic system for unsteady pressure measurements using conventional sensors /

Abstract

Extracted data

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