Equations for the induced velocities near a lifitng rotor with nonuniform azimuthwise vorticity distribution /

Aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with the rotors removed /

Mineck, Raymond E.
Hassell, James L., joint author.
Freeman, Carl E., joint author.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

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...

Flight measurements of the effects of blade out of track on the vibration levels on a tandem rotor helicopter /

United States. National Aeronautics and Space Administration.
Langley Research Center.

"May 1960."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Tables and charts of the normal component of induced velocity in the lateral plane of a rotor with harmonic azimuthwise vorticity distribution /

Heyson, Harry H.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Propulsion systems, air-jet.Includes bibliographical references.Mode of acc...

Measurements of the time-averaged and instantaneous induced velocities in the wake of a helicopter rotor hovering at high tip speeds /

Heyson, Harry H.
United States. National Aeronautics and Space Administration.

Cover title."July 1960."Aircraft; Propulsion systems, air-jet.Includes bibliographical references.Mo...

Some recent studies in structural dynamics of rotor aircraft /

Brooks, George W.
Silveira, Milton A.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aircraft; Propulsion systems, air-jet; Stresses and loads.Includes bibliogr...

Aerodynamic loads on an isolated shrouded-propeller configuration of angles of attack from -10 degrees to 110 degrees /

Grunwald, Kalman J.
Goodson, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bi...

Hovering measurements for twin-rotor configurations with and without overlap /

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

Cover title."November 1960."Aerodynamics, aircraft; Propulsion systems, air-jet.Includes bibliograph...

Experimental and calculated flow fields produced by airplanes flying at supersonic speeds /

Smith, Harriet J.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics aircraft; Aircraft safety and noise.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...

Considerations of methods of improving helicopter efficiency /

Dingeldein, Richard C.
United States. National Aeronautics and Space Administration.

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

Shock-wave patterns on a cranked-wing configuration /

Sammonds, Robert I.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles.Includ...

Flight investigation of effects of selected operatings conditions on the bending and torsional moments encountered by a helicopter rotor blade /

Ludi, LeRoy H.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aircraft; Propulsion systems, air-jet; Stresses and loads.Includes bibliogr...

An investigation of periodic forces and moments transmitted to the hub of the four lifting rotor configurations /

Silveira, Milton A.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Propulsion systems, air-jet; Stresses and loads.Includes bibliographical re...

Axial-force reduction by interference between jet and neighboring afterbody /

Pitts, William C.
Wiggins, Lyle E.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, missiles and space vehicles.Includes bibliographical refe...

Aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with the rotors removed /

Mineck, Raymond E.
Hassell, James L., joint author.
Freeman, Carl E., joint author.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

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...

Flight measurements of the effects of blade out of track on the vibration levels on a tandem rotor helicopter /

United States. National Aeronautics and Space Administration.
Langley Research Center.

"May 1960."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Tables and charts of the normal component of induced velocity in the lateral plane of a rotor with harmonic azimuthwise vorticity distribution /

Heyson, Harry H.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Propulsion systems, air-jet.Includes bibliographical references.Mode of acc...

Measurements of the time-averaged and instantaneous induced velocities in the wake of a helicopter rotor hovering at high tip speeds /

Heyson, Harry H.
United States. National Aeronautics and Space Administration.

Cover title."July 1960."Aircraft; Propulsion systems, air-jet.Includes bibliographical references.Mo...

Some recent studies in structural dynamics of rotor aircraft /

Brooks, George W.
Silveira, Milton A.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aircraft; Propulsion systems, air-jet; Stresses and loads.Includes bibliogr...

Aerodynamic loads on an isolated shrouded-propeller configuration of angles of attack from -10 degrees to 110 degrees /

Grunwald, Kalman J.
Goodson, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bi...

Hovering measurements for twin-rotor configurations with and without overlap /

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

Cover title."November 1960."Aerodynamics, aircraft; Propulsion systems, air-jet.Includes bibliograph...

Experimental and calculated flow fields produced by airplanes flying at supersonic speeds /

Smith, Harriet J.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics aircraft; Aircraft safety and noise.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...

Considerations of methods of improving helicopter efficiency /

Dingeldein, Richard C.
United States. National Aeronautics and Space Administration.

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

Shock-wave patterns on a cranked-wing configuration /

Sammonds, Robert I.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles.Includ...

Flight investigation of effects of selected operatings conditions on the bending and torsional moments encountered by a helicopter rotor blade /

Ludi, LeRoy H.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aircraft; Propulsion systems, air-jet; Stresses and loads.Includes bibliogr...

An investigation of periodic forces and moments transmitted to the hub of the four lifting rotor configurations /

Silveira, Milton A.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Propulsion systems, air-jet; Stresses and loads.Includes bibliographical re...

Axial-force reduction by interference between jet and neighboring afterbody /

Pitts, William C.
Wiggins, Lyle E.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, missiles and space vehicles.Includes bibliographical refe...

Aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with the rotors removed /

Mineck, Raymond E.
Hassell, James L., joint author.
Freeman, Carl E., joint author.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

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...

Flight measurements of the effects of blade out of track on the vibration levels on a tandem rotor helicopter /

United States. National Aeronautics and Space Administration.
Langley Research Center.

"May 1960."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Equations for the induced velocities near a lifitng rotor with nonuniform azimuthwise vorticity distribution /

Abstract

Extracted data

Equations for the induced velocities near a lifitng rotor with nonuniform azimuthwise vorticity distribution /

Abstract

Extracted data

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