Light airplane crash tests at three roll angles /

Emergency in-flight egress opening for general aviation aircraft /

Bement, Laurence J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Subject category 05."April 1980"--Cover."Langley Research Center."Includes bibliographical reference...

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...

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...

Full-scale crash-test evaluation of two load-limiting subfloors for general aviation airframes /

Carden, Huey D.
Langley Research Center.

January 1984

Prepared at Langley Research Center."December 1984"--Cover.Includes bibliographical references (p. 1...

Impact data from a transport aircraft during a controlled impact demonstration /

Fasanella, Edwin L.
Hayduk, Robert J.
Alfaro-Bou, Emilio.
Langley Research Center.

January 1986

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

Evaluation of emergency-locator-transmitter performance in real and simulated crash tests /

Carden, Huey D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 39."April 1981"--Cover."Langley Research Center."Includes bibliographical reference...

Analytical investigation of the landing dynamics of a large airplane with a load-control system in the main landing gear /

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

January 1979

"Langley Research Center.""December 1979"--Cover.Includes bibliographical references.Mode of access:...

Spin tests of a single-engine, high-wing light airplane /

Stewart, Eric C.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject category 05."Langley Research Center.""January 1982"--Cover.Includes bibliographical referen...

Flight test of a pitch control for a spinning vehicle /

Garner, H. Douglas.
Reid, H. J. E.
Langley Research Center.

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

The landing flare : an analysis and flight-test investigation /

Seckel, Edward, 1921-2009.
Langley Research Center.
Princeton University. Flight Research Laboratory.

"Prepared by Princeton University, [Flight Research Laboratory] ... for Langley Research Center.""Ma...

Airline pilot scan patterns during simulated ILS approaches /

Spady, Amos A.
Langley Research Center.

January 1978

Prepared at Langley Research Center."October 1978"--Cover.Includes bibliographical references (p. 38...

Experimental study of acoustic loads on upper-surface-blown STOL airplane configuration /

Willis, Conrad M.
Schoenster, James A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"Langley Research Center.""December 1979"--Cover.Includes bibliographical references.Mode of access:...

Analytical modeling of transport aircraft crash scenarios to obtain floor pulses /

Lackey, Dave.
Wittlin, Gil.
Federal Aviation Administration Technical Center (U.S.)
United States. National Aeronautics and Space Administration.
United States. Federal Aviation Administration. Systems Research and Development Service.
Lockheed-California Company.

"April 1983."Cover title.Includes bibliographical references.Sponsored by National Aeronautics and S...

Crash tests of three identical low-wing single-engine airplanes /

Castle, Claude B.
Alfaro-Bou, Emilio.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 03."September 1983"--Cover.Distributed to depository libraries in microfiche.Includ...

Flight investigation of the effects of an outboard wing-leading-edge modification on stall/spin characteristics of a low-wing, single-engine, T-tail light airplane /

Stough, H. Paul.
Patton, James M., Jr.
DiCarlo, Daniel J.
Langley Research Center.

January 1987

Prepared at Langley Research Center."July 1987"--Cover.Includes bibliographical references (p. 9).Mo...

Emergency in-flight egress opening for general aviation aircraft /

Bement, Laurence J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Subject category 05."April 1980"--Cover."Langley Research Center."Includes bibliographical reference...

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...

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...

Full-scale crash-test evaluation of two load-limiting subfloors for general aviation airframes /

Carden, Huey D.
Langley Research Center.

January 1984

Prepared at Langley Research Center."December 1984"--Cover.Includes bibliographical references (p. 1...

Impact data from a transport aircraft during a controlled impact demonstration /

Fasanella, Edwin L.
Hayduk, Robert J.
Alfaro-Bou, Emilio.
Langley Research Center.

January 1986

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

Evaluation of emergency-locator-transmitter performance in real and simulated crash tests /

Carden, Huey D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 39."April 1981"--Cover."Langley Research Center."Includes bibliographical reference...

Analytical investigation of the landing dynamics of a large airplane with a load-control system in the main landing gear /

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

January 1979

"Langley Research Center.""December 1979"--Cover.Includes bibliographical references.Mode of access:...

Spin tests of a single-engine, high-wing light airplane /

Stewart, Eric C.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject category 05."Langley Research Center.""January 1982"--Cover.Includes bibliographical referen...

Flight test of a pitch control for a spinning vehicle /

Garner, H. Douglas.
Reid, H. J. E.
Langley Research Center.

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

The landing flare : an analysis and flight-test investigation /

Seckel, Edward, 1921-2009.
Langley Research Center.
Princeton University. Flight Research Laboratory.

"Prepared by Princeton University, [Flight Research Laboratory] ... for Langley Research Center.""Ma...

Airline pilot scan patterns during simulated ILS approaches /

Spady, Amos A.
Langley Research Center.

January 1978

Prepared at Langley Research Center."October 1978"--Cover.Includes bibliographical references (p. 38...

Experimental study of acoustic loads on upper-surface-blown STOL airplane configuration /

Willis, Conrad M.
Schoenster, James A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"Langley Research Center.""December 1979"--Cover.Includes bibliographical references.Mode of access:...

Analytical modeling of transport aircraft crash scenarios to obtain floor pulses /

Lackey, Dave.
Wittlin, Gil.
Federal Aviation Administration Technical Center (U.S.)
United States. National Aeronautics and Space Administration.
United States. Federal Aviation Administration. Systems Research and Development Service.
Lockheed-California Company.

"April 1983."Cover title.Includes bibliographical references.Sponsored by National Aeronautics and S...

Crash tests of three identical low-wing single-engine airplanes /

Castle, Claude B.
Alfaro-Bou, Emilio.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 03."September 1983"--Cover.Distributed to depository libraries in microfiche.Includ...

Flight investigation of the effects of an outboard wing-leading-edge modification on stall/spin characteristics of a low-wing, single-engine, T-tail light airplane /

Stough, H. Paul.
Patton, James M., Jr.
DiCarlo, Daniel J.
Langley Research Center.

January 1987

Prepared at Langley Research Center."July 1987"--Cover.Includes bibliographical references (p. 9).Mo...

Emergency in-flight egress opening for general aviation aircraft /

Bement, Laurence J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Subject category 05."April 1980"--Cover."Langley Research Center."Includes bibliographical reference...

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...

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...

Light airplane crash tests at three roll angles /

Abstract

Extracted data

Light airplane crash tests at three roll angles /

Abstract

Extracted data

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