Experimental investigation of active loads control for aircraft landing gear /

Flutter clearance of the horizontal tail of the Bellanca Skyrocket II airplane /

Ricketts, Rodney H.
Farmer, Moses G.
Cazier, F. W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

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

Low-speed tests of an all-flexible parawing for landing a lifting-body spacecraft /

Bugg, Frank M.
Sleeman, William C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 12).Mode of access: Internet

Application of the concept of dynamic trim control to automatic landing of Carrier aircraft /

Smith, Allan G.
Meyer, George.
Ames Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"Ames Research Center.""April 1980"--Cover.Includes bibliographical references.Mode of access: Inter...

An Electronic control for an electrohydraulic active control aircraft landind gear /

Ross, Irving.
Edson, Ralph.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

"April 1979"--Cover.Includes bibliographical references.Mode of access: Internet

A mathematical model of an active control landing gear for load control during impact and roll-out /

McGehee, John R.
Carden, Huey D.
Langley Research Center.

January 1976

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 42).Mode of ...

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:...

Experimental investigation of the use of soft side legs to improve touchdown stability of legged landing vehicles /

Herr, Robert W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."August 1968."Includes bibliographical references (p. 8).Mode of access: Internet

Experimental and analytical studies of advanced air cushion landing systems /

Lee, E. G. S.
Langley Research Center.
Foster-Miller Associates.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

"Foster-Miller Associates, Inc.""November 1981"--Cover.Includes bibliographical references.Mode of a...

Investigation over moving ground plane of a transport airplane model using blowing over flaps for boundary-layer control /

Vogler, Raymond D.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 10).Mode of access: Internet

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:...

Experimental investigation of advanced concepts to increase turbine blade loading.

Lueders, H. G. (Howard George)

"April 1969"--cover.Includes bibliographical references.Mode of access: Internet

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. ...

Investigation of the landing characteristics of a reentry vehicle having a canted multiple-air-bag load-alleviation system /

Stubbs, Sandy M.
McGehee, John R.
United States. National Aeronautics and Space Administration.

Cover title."August 1963."Includes bibliographical references.Mode of access: Internet

Static investigation of several jet deflectors for longitudinal control of an aircraft /

Valerino, Alfred S.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "June 7, 1955."Title from cover.Includes bibliographical references: p. 9.Mode of ac...

Flight control systems development and flight test experience with the HiMAT research vehicles /

Kempel, Robert W.
Earls, Michael R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"June 1988"--Cover.Includes bibliographical references (p. 25).Mode of access: Internet

Flutter clearance of the horizontal tail of the Bellanca Skyrocket II airplane /

Ricketts, Rodney H.
Farmer, Moses G.
Cazier, F. W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

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

Low-speed tests of an all-flexible parawing for landing a lifting-body spacecraft /

Bugg, Frank M.
Sleeman, William C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 12).Mode of access: Internet

Application of the concept of dynamic trim control to automatic landing of Carrier aircraft /

Smith, Allan G.
Meyer, George.
Ames Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"Ames Research Center.""April 1980"--Cover.Includes bibliographical references.Mode of access: Inter...

An Electronic control for an electrohydraulic active control aircraft landind gear /

Ross, Irving.
Edson, Ralph.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

"April 1979"--Cover.Includes bibliographical references.Mode of access: Internet

A mathematical model of an active control landing gear for load control during impact and roll-out /

McGehee, John R.
Carden, Huey D.
Langley Research Center.

January 1976

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 42).Mode of ...

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:...

Experimental investigation of the use of soft side legs to improve touchdown stability of legged landing vehicles /

Herr, Robert W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."August 1968."Includes bibliographical references (p. 8).Mode of access: Internet

Experimental and analytical studies of advanced air cushion landing systems /

Lee, E. G. S.
Langley Research Center.
Foster-Miller Associates.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

"Foster-Miller Associates, Inc.""November 1981"--Cover.Includes bibliographical references.Mode of a...

Investigation over moving ground plane of a transport airplane model using blowing over flaps for boundary-layer control /

Vogler, Raymond D.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 10).Mode of access: Internet

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:...

Experimental investigation of advanced concepts to increase turbine blade loading.

Lueders, H. G. (Howard George)

"April 1969"--cover.Includes bibliographical references.Mode of access: Internet

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. ...

Investigation of the landing characteristics of a reentry vehicle having a canted multiple-air-bag load-alleviation system /

Stubbs, Sandy M.
McGehee, John R.
United States. National Aeronautics and Space Administration.

Cover title."August 1963."Includes bibliographical references.Mode of access: Internet

Static investigation of several jet deflectors for longitudinal control of an aircraft /

Valerino, Alfred S.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "June 7, 1955."Title from cover.Includes bibliographical references: p. 9.Mode of ac...

Flight control systems development and flight test experience with the HiMAT research vehicles /

Kempel, Robert W.
Earls, Michael R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"June 1988"--Cover.Includes bibliographical references (p. 25).Mode of access: Internet

Flutter clearance of the horizontal tail of the Bellanca Skyrocket II airplane /

Ricketts, Rodney H.
Farmer, Moses G.
Cazier, F. W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

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

Low-speed tests of an all-flexible parawing for landing a lifting-body spacecraft /

Bugg, Frank M.
Sleeman, William C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 12).Mode of access: Internet

Application of the concept of dynamic trim control to automatic landing of Carrier aircraft /

Smith, Allan G.
Meyer, George.
Ames Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"Ames Research Center.""April 1980"--Cover.Includes bibliographical references.Mode of access: Inter...

Experimental investigation of active loads control for aircraft landing gear /

Abstract

Extracted data

Experimental investigation of active loads control for aircraft landing gear /

Abstract

Extracted data

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