Effect of a variable camber and twist wing at transonic Mach numbers /

Calculation of the twist distribution of wings designed for cruise at transonic speeds /

Mann, Michael J.
Langley Research Center.

January 1974

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

Chang, I-Chung.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1990

"June 1990."Cover title.Distributed to depository libraries in microfiche.Includes bibliographical r...

Effects of wing incidence on the longitudinal trim characteristics of a cambered 70° delta-wing configuration at mach numbers 3.0 to 5.0 /

Ahtye, Warren F.
Ames Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

Body and canard effects on an attached-flow maneuver wing at Mach 1.62 /

Pittman, Jimmy L.
Mason, William H. (William Henry), 1947-
Miller, David S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

"February 1984"--Cover.Distributed to depository libraries in microfiche.Includes bibliographical re...

Wing planform effects at supersonic speeds for an advanced fighter configuration /

Wood, Richard M.
Miller, D. S. (David S.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

"March 1984"--Cover.Distributed to depository libraries in microfiche.Subject category 02.Includes b...

Aerodynamic characteristics of a series of bodies with variations in nose camber /

Shrout, Barrett L.
Covell, Peter F.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche."September 1983"--Cover.Includes bibliographical r...

Low-speed aerodynamic characteristics of a highly swept, untwisted, uncambered arrow wing /

Coe, Paul L.
Gentry, Garl L.
Kjelgaard, Scott O.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche."October 1983"--Cover.Includes bibliographical ref...

Aerodynamic characteristics, including effect of body shape, of a Mach 6 aircraft concept /

Riebe, Gregory D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 02."December 1983"--Cover.Distributed to depository libraries in microfiche.Include...

Effect on empennage location on twin-engine afterbody/nozzle aerodynamic characteristics at Mach numbers from 0.6 to 1.2 /

Leavitt, Laurence D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche."May 1983"--Cover.Includes bibliographical referen...

Effects of configuration modifications on aerodynamic characteristics of tension shell shapes at Mach 3.0 /

Sawyer, James Wayne, 1941-
Deveikis, William D.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 11).Mode of access: Internet

Numerical studies of the deposition of material released from fixed and rotary wing aircraft /

Bilanin, Alan J.
Teske, Milton E.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1984

"March 1984"--Cover.Subject category-02.Distributed to depository libraries in microfiche.Includes b...

Effects of deflected wing tips on the aerodynamic characteristics of a canard configuration at mach numbers from 0.7 to 3.5 /

Peterson, Victor L.
Bright, Loren G.
Ames Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 21).Mode of access: Internet

Effects of winglet on transonic flutter characteristics of a cantilevered twin-engine-transport wing model /

Ruhlin, Charles L.
Nagaraja, K. S.
Bhatia, Kumar G. (Kumar Gobindram), 1941-
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986"--Cover.Includes bibliographical references (p. 2...

Interference effects of canard controls on the longitudinal aerodynamic characteristics of a winged body at Mach 10 /

Brooks, Cuyler W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 11).Mode of access: Internet

Downwash in the plane of symmetry of an elliptically loaded wing /

Phillips, James D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1985

Distributed to depository libraries in microfiche.Subject category 2."January 1985"--Cover.Includes ...

Calculation of the twist distribution of wings designed for cruise at transonic speeds /

Mann, Michael J.
Langley Research Center.

January 1974

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

Transonic flow analysis for rotors.

Chang, I-Chung.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1990

"June 1990."Cover title.Distributed to depository libraries in microfiche.Includes bibliographical r...

Effects of wing incidence on the longitudinal trim characteristics of a cambered 70° delta-wing configuration at mach numbers 3.0 to 5.0 /

Ahtye, Warren F.
Ames Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

Body and canard effects on an attached-flow maneuver wing at Mach 1.62 /

Pittman, Jimmy L.
Mason, William H. (William Henry), 1947-
Miller, David S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

"February 1984"--Cover.Distributed to depository libraries in microfiche.Includes bibliographical re...

Wing planform effects at supersonic speeds for an advanced fighter configuration /

Wood, Richard M.
Miller, D. S. (David S.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

"March 1984"--Cover.Distributed to depository libraries in microfiche.Subject category 02.Includes b...

Aerodynamic characteristics of a series of bodies with variations in nose camber /

Shrout, Barrett L.
Covell, Peter F.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche."September 1983"--Cover.Includes bibliographical r...

Low-speed aerodynamic characteristics of a highly swept, untwisted, uncambered arrow wing /

Coe, Paul L.
Gentry, Garl L.
Kjelgaard, Scott O.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche."October 1983"--Cover.Includes bibliographical ref...

Aerodynamic characteristics, including effect of body shape, of a Mach 6 aircraft concept /

Riebe, Gregory D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 02."December 1983"--Cover.Distributed to depository libraries in microfiche.Include...

Effect on empennage location on twin-engine afterbody/nozzle aerodynamic characteristics at Mach numbers from 0.6 to 1.2 /

Leavitt, Laurence D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche."May 1983"--Cover.Includes bibliographical referen...

Effects of configuration modifications on aerodynamic characteristics of tension shell shapes at Mach 3.0 /

Sawyer, James Wayne, 1941-
Deveikis, William D.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 11).Mode of access: Internet

Numerical studies of the deposition of material released from fixed and rotary wing aircraft /

Bilanin, Alan J.
Teske, Milton E.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1984

"March 1984"--Cover.Subject category-02.Distributed to depository libraries in microfiche.Includes b...

Effects of deflected wing tips on the aerodynamic characteristics of a canard configuration at mach numbers from 0.7 to 3.5 /

Peterson, Victor L.
Bright, Loren G.
Ames Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 21).Mode of access: Internet

Effects of winglet on transonic flutter characteristics of a cantilevered twin-engine-transport wing model /

Ruhlin, Charles L.
Nagaraja, K. S.
Bhatia, Kumar G. (Kumar Gobindram), 1941-
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986"--Cover.Includes bibliographical references (p. 2...

Interference effects of canard controls on the longitudinal aerodynamic characteristics of a winged body at Mach 10 /

Brooks, Cuyler W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 11).Mode of access: Internet

Downwash in the plane of symmetry of an elliptically loaded wing /

Phillips, James D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1985

Distributed to depository libraries in microfiche.Subject category 2."January 1985"--Cover.Includes ...

Calculation of the twist distribution of wings designed for cruise at transonic speeds /

Mann, Michael J.
Langley Research Center.

January 1974

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

Transonic flow analysis for rotors.

Chang, I-Chung.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1990

"June 1990."Cover title.Distributed to depository libraries in microfiche.Includes bibliographical r...

Effects of wing incidence on the longitudinal trim characteristics of a cambered 70° delta-wing configuration at mach numbers 3.0 to 5.0 /

Ahtye, Warren F.
Ames Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

Effect of a variable camber and twist wing at transonic Mach numbers /

Abstract

Extracted data

Effect of a variable camber and twist wing at transonic Mach numbers /

Abstract

Extracted data

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