Aerodynamic characteristics of two rotorcraft airfoils designed for application to the inboard region of a main rotor blade /

Effect of blade planform variation on the forward-flight performance of small-scale rotors /

Noonan, Kevin W.
United States. Army. Aeroflightdynamics Directorate.

January 1992

Prepared at the U.S. Army Aeroflightdynamics Directorate.Includes bibliographical references (p. 6-7...

Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 /

Noonan, Kevin W.
Bingham, Gene J.
Army Research and Technology Laboratories (U.S.). Structures Laboratory.
United States. Army Aviation Research and Development Command.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Sept. 1980."U.S. Army AVRADCOM"--Cover."Structures Laboratory, AVRADCOM Research and Technology Labo...

Aerodynamic characteristics of three slender sharp-edge 74 ̊swept wings at subsonic, transonic, and supersonic Mach numbers /

Davenport, Edwin E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 9).Mode of a...

An analytical evaluation of airfoil sections for helicopter rotor applications /

Bingham, Gene J.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode ...

Low-speed aerodynamic characteristics of an airfoil optimized for maximum lift coefficient /

Bingham, Gene J.
Chen, Allen Wen-shin, 1945-
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 13.Mode of access: Internet

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...

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

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

Effect of advanced rotorcraft airfoil sections on the hover performance of a small-scale rotor model /

Althoff, Susan L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"September 1988"--Cover.Includes bibliographical references (p. 7-8).Mode of access: Internet

Aerodynamic performance of a 0.27-scale model of an AH-64 helicopter with baseline and alternate rotor blade sets /

Kelley, Henry L.
United States. Army Aerostructures Directorate.

January 1990

Prepared at the Aerostructures Directorate, USAARTA-AVSCOM, Langley Research Center.Bibliography: p....

Performance data from a wind-tunnel test of two main-rotor blade designs for a utility-class helicopter /

Singleton, Jeffrey D.
Wilbur, Matthew L.
Yeager, William T.
United States. Army Aerostructures Directorate.

January 1990

Prepared at the Army Aerostructures Directorate, USAARTA-AVSCOM, Langley Research Center.Bibliograph...

Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers /

Dunham, Dana Morris.
Langley Research Center.

January 1987

Prepared at Langley Research Center."October 1987"--Cover.Includes bibliographical references (p. 57...

Effect of blade planform variation on a small-scale hovering rotor /

Althoff, Susan L.
Noonan, Kevin W.
United States. Army Aerostructures Directorate.

January 1990

Research done at Aerostrucures Directorate, USAARTA-AVSCOM, Langley Research Center.Bibliography: p....

Performance of an optimized rotor blade at off-design flight conditions /

Chattopadhyay, Aditi, 1958-
Langley Research Center.
Analytical Services & Materials, Inc.

January 1990

Prepared at Analytical Services & Materials, Inc., for Langley Research Center under Contract NAS1-1...

Aerodynamic characteristics of wings designed with a combined-theory method to cruise at a Mach number of 4.5 /

Mack, Robert J.
Langley Research Center.

January 1988

Prepared at Langley Research Center."April 1988"--Cover.Includes bibliographical references (p. 10-1...

Effect of blade planform variation on the forward-flight performance of small-scale rotors /

Noonan, Kevin W.
United States. Army. Aeroflightdynamics Directorate.

January 1992

Prepared at the U.S. Army Aeroflightdynamics Directorate.Includes bibliographical references (p. 6-7...

Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 /

Noonan, Kevin W.
Bingham, Gene J.
Army Research and Technology Laboratories (U.S.). Structures Laboratory.
United States. Army Aviation Research and Development Command.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Sept. 1980."U.S. Army AVRADCOM"--Cover."Structures Laboratory, AVRADCOM Research and Technology Labo...

Aerodynamic characteristics of three slender sharp-edge 74 ̊swept wings at subsonic, transonic, and supersonic Mach numbers /

Davenport, Edwin E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 9).Mode of a...

An analytical evaluation of airfoil sections for helicopter rotor applications /

Bingham, Gene J.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode ...

Low-speed aerodynamic characteristics of an airfoil optimized for maximum lift coefficient /

Bingham, Gene J.
Chen, Allen Wen-shin, 1945-
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 13.Mode of access: Internet

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...

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

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

Effect of advanced rotorcraft airfoil sections on the hover performance of a small-scale rotor model /

Althoff, Susan L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"September 1988"--Cover.Includes bibliographical references (p. 7-8).Mode of access: Internet

Aerodynamic performance of a 0.27-scale model of an AH-64 helicopter with baseline and alternate rotor blade sets /

Kelley, Henry L.
United States. Army Aerostructures Directorate.

January 1990

Prepared at the Aerostructures Directorate, USAARTA-AVSCOM, Langley Research Center.Bibliography: p....

Performance data from a wind-tunnel test of two main-rotor blade designs for a utility-class helicopter /

Singleton, Jeffrey D.
Wilbur, Matthew L.
Yeager, William T.
United States. Army Aerostructures Directorate.

January 1990

Prepared at the Army Aerostructures Directorate, USAARTA-AVSCOM, Langley Research Center.Bibliograph...

Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers /

Dunham, Dana Morris.
Langley Research Center.

January 1987

Prepared at Langley Research Center."October 1987"--Cover.Includes bibliographical references (p. 57...

Effect of blade planform variation on a small-scale hovering rotor /

Althoff, Susan L.
Noonan, Kevin W.
United States. Army Aerostructures Directorate.

January 1990

Research done at Aerostrucures Directorate, USAARTA-AVSCOM, Langley Research Center.Bibliography: p....

Performance of an optimized rotor blade at off-design flight conditions /

Chattopadhyay, Aditi, 1958-
Langley Research Center.
Analytical Services & Materials, Inc.

January 1990

Prepared at Analytical Services & Materials, Inc., for Langley Research Center under Contract NAS1-1...

Aerodynamic characteristics of wings designed with a combined-theory method to cruise at a Mach number of 4.5 /

Mack, Robert J.
Langley Research Center.

January 1988

Prepared at Langley Research Center."April 1988"--Cover.Includes bibliographical references (p. 10-1...

Effect of blade planform variation on the forward-flight performance of small-scale rotors /

Noonan, Kevin W.
United States. Army. Aeroflightdynamics Directorate.

January 1992

Prepared at the U.S. Army Aeroflightdynamics Directorate.Includes bibliographical references (p. 6-7...

Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 /

Noonan, Kevin W.
Bingham, Gene J.
Army Research and Technology Laboratories (U.S.). Structures Laboratory.
United States. Army Aviation Research and Development Command.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Sept. 1980."U.S. Army AVRADCOM"--Cover."Structures Laboratory, AVRADCOM Research and Technology Labo...

Aerodynamic characteristics of three slender sharp-edge 74 ̊swept wings at subsonic, transonic, and supersonic Mach numbers /

Davenport, Edwin E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 9).Mode of a...

Aerodynamic characteristics of two rotorcraft airfoils designed for application to the inboard region of a main rotor blade /

Abstract

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Aerodynamic characteristics of two rotorcraft airfoils designed for application to the inboard region of a main rotor blade /

Abstract

Extracted data

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