A Wind-tunnel investigation of the longitudinal aerodynamic charachteristics of two full-scale helicopter fuselage models with appendages / Julian L. Jenkins, Matthew M. Winston and George E. Sweet.

An experimental investigation of the effect of wind tunnel walls on the aerodynamic performance of a helicopter rotor /

Ganzer, Victor M.
Rae, William H.
University of Washington.

January 1960

"NASA TN D-415.""University of Washington.""May 1960."Cover title.Includes bibliographical reference...

A tabulation of wind-tunnel pressure data and section aerodynamic characteristics at Mach numbers of 1.61 and 2.01 for two trapezoidal and three delta wings having different surface shapes /

Landrum, Emma Jean.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft;Stresses and loads.Includes bibliograp...

Hovering characteristics of a rotor having an airfoil section designed for a utility type of helicopter y James P. Shivers and William J. Monahan.

Shivers, James P.
Monahan, William J.
United States. National Aeronautics and Space Administration.

Cover title."December 1962."Includes bibliographical references.Mode of access: Internet

Wind-tunnel investigating of the drag and static stability characteristics of four helicopter fuselage models / George E. Sweet and Julian L. Jenkins Jr.

Sweet, George E.
Jenkins, Julian L.
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mode of...

A wind-tunnel investigation at a Mach number of 2.01 of the sonic-boom characteristics of three wing-body combinations differing in wing longitudinal location /

Morris, Odell A.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise.Includes bi...

Low-speed wind-tunnel investigation to determine the flight characteristics of a model of a parawing utility vehicle. Joseph L. Johnson.

Johnson, Joseph L.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliogra...

wind-tunnel investigation of longitudinal aerodynamic characteristics of three propeller-driven VTOL configurations in the transition speed range, including effects of ground proximity /

Kuhn, Richard E.
Hayes, William C.
United States. National Aeronautics and Space Administration.

Cover title."February 1960."Flaps, trailing-edge, complete wings; Slipstream, propellers; Tail-wing-...

Wind-tunnel investigation of the effects of wing bodies, fences, flaps, and fuselage addition on the wing buffet response of a transonic-transport model /

Cornette, Elden S.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referen...

Wind-tunnel investigation of tail buffet at subsonic and transonic speeds employing a dynamic elastic aircraft model / Robert N. Rigby and Elden S. Cornette.

Rigby, Robert N.
Cornette, Elden S.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical ref...

Wind-tunnel investigation of a small-scale model of an aerial vehicle supported by tilting ducted fans /

Smith, Charles C.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft; Stability and control.Includes bibliographical ref...

Full scale wind-tunnel tests of blowing boundary-layer control applied to a helicopter rotor /

McCloud, John L.
Brady, James A.
Hall, Leo P.
United States. National Aeronautics and Space Administration.

Cover title." September 1960."Aircraft; Propulsion systems, air-jet.Includes bibliographical referen...

Full-scale wind-tunnel investigation of the aerodynamic characteristics of the X-24A lifting body aircraft /

Mort, Kenneth W.
Falarski, Michael D.
U.S. Army Aeronautical Research Laboratory.
Ames Research Center.
United States. National Aeronautics and Space Administration.

"August 1970."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

A WIND-TUNNEL INVESTIGATION OF THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF TWO FULL-SCALE HELICOPTER FUSELAGE MODELS WITH APPENDAGES

Winston, M. M.
Sweet, G. E.
Jenkins, J. L., Jr.

July 1962

Longitudinal aerodynamic characteristics of two full-scale helicopter fuselage model

A Wind-tunnel investigation of pressure fluctuations on the upper vertical tail of the X-15 when mated to the B-52 carrier airplane / John W. McKee and Thomas A. Byrdsong.

McKee, John W.
Byrdsong, Thomas A.
United States. National Aeronautics and Space Administration.

Cover title."June 1962."Aerodynamics, aircraft; Aircraft; Stresses and loads.Includes bibliographica...

Hovering characteristics of a rotor having an airfoil section designed for flying-crane type of helicopter /

Shivers, James P.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bibl...

An experimental investigation of the effect of wind tunnel walls on the aerodynamic performance of a helicopter rotor /

Ganzer, Victor M.
Rae, William H.
University of Washington.

January 1960

"NASA TN D-415.""University of Washington.""May 1960."Cover title.Includes bibliographical reference...

A tabulation of wind-tunnel pressure data and section aerodynamic characteristics at Mach numbers of 1.61 and 2.01 for two trapezoidal and three delta wings having different surface shapes /

Landrum, Emma Jean.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft;Stresses and loads.Includes bibliograp...

Hovering characteristics of a rotor having an airfoil section designed for a utility type of helicopter y James P. Shivers and William J. Monahan.

Shivers, James P.
Monahan, William J.
United States. National Aeronautics and Space Administration.

Cover title."December 1962."Includes bibliographical references.Mode of access: Internet

Wind-tunnel investigating of the drag and static stability characteristics of four helicopter fuselage models / George E. Sweet and Julian L. Jenkins Jr.

Sweet, George E.
Jenkins, Julian L.
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mode of...

A wind-tunnel investigation at a Mach number of 2.01 of the sonic-boom characteristics of three wing-body combinations differing in wing longitudinal location /

Morris, Odell A.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise.Includes bi...

Low-speed wind-tunnel investigation to determine the flight characteristics of a model of a parawing utility vehicle. Joseph L. Johnson.

Johnson, Joseph L.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliogra...

wind-tunnel investigation of longitudinal aerodynamic characteristics of three propeller-driven VTOL configurations in the transition speed range, including effects of ground proximity /

Kuhn, Richard E.
Hayes, William C.
United States. National Aeronautics and Space Administration.

Cover title."February 1960."Flaps, trailing-edge, complete wings; Slipstream, propellers; Tail-wing-...

Wind-tunnel investigation of the effects of wing bodies, fences, flaps, and fuselage addition on the wing buffet response of a transonic-transport model /

Cornette, Elden S.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referen...

Wind-tunnel investigation of tail buffet at subsonic and transonic speeds employing a dynamic elastic aircraft model / Robert N. Rigby and Elden S. Cornette.

Rigby, Robert N.
Cornette, Elden S.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical ref...

Wind-tunnel investigation of a small-scale model of an aerial vehicle supported by tilting ducted fans /

Smith, Charles C.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft; Stability and control.Includes bibliographical ref...

Full scale wind-tunnel tests of blowing boundary-layer control applied to a helicopter rotor /

McCloud, John L.
Brady, James A.
Hall, Leo P.
United States. National Aeronautics and Space Administration.

Cover title." September 1960."Aircraft; Propulsion systems, air-jet.Includes bibliographical referen...

Full-scale wind-tunnel investigation of the aerodynamic characteristics of the X-24A lifting body aircraft /

Mort, Kenneth W.
Falarski, Michael D.
U.S. Army Aeronautical Research Laboratory.
Ames Research Center.
United States. National Aeronautics and Space Administration.

"August 1970."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

A WIND-TUNNEL INVESTIGATION OF THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF TWO FULL-SCALE HELICOPTER FUSELAGE MODELS WITH APPENDAGES

Winston, M. M.
Sweet, G. E.
Jenkins, J. L., Jr.

July 1962

Longitudinal aerodynamic characteristics of two full-scale helicopter fuselage model

A Wind-tunnel investigation of pressure fluctuations on the upper vertical tail of the X-15 when mated to the B-52 carrier airplane / John W. McKee and Thomas A. Byrdsong.

McKee, John W.
Byrdsong, Thomas A.
United States. National Aeronautics and Space Administration.

Cover title."June 1962."Aerodynamics, aircraft; Aircraft; Stresses and loads.Includes bibliographica...

Hovering characteristics of a rotor having an airfoil section designed for flying-crane type of helicopter /

Shivers, James P.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bibl...

An experimental investigation of the effect of wind tunnel walls on the aerodynamic performance of a helicopter rotor /

Ganzer, Victor M.
Rae, William H.
University of Washington.

January 1960

"NASA TN D-415.""University of Washington.""May 1960."Cover title.Includes bibliographical reference...

A tabulation of wind-tunnel pressure data and section aerodynamic characteristics at Mach numbers of 1.61 and 2.01 for two trapezoidal and three delta wings having different surface shapes /

Landrum, Emma Jean.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft;Stresses and loads.Includes bibliograp...

Hovering characteristics of a rotor having an airfoil section designed for a utility type of helicopter y James P. Shivers and William J. Monahan.

Shivers, James P.
Monahan, William J.
United States. National Aeronautics and Space Administration.

Cover title."December 1962."Includes bibliographical references.Mode of access: Internet

A Wind-tunnel investigation of the longitudinal aerodynamic charachteristics of two full-scale helicopter fuselage models with appendages / Julian L. Jenkins, Matthew M. Winston and George E. Sweet.

Abstract

Extracted data

A Wind-tunnel investigation of the longitudinal aerodynamic charachteristics of two full-scale helicopter fuselage models with appendages / Julian L. Jenkins, Matthew M. Winston and George E. Sweet.

Abstract

Extracted data

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