Ask
Search
My library
ORKG

ORKG Ask

Our mission is to organize scholarly knowledge and make it accessible to humans and machines.

About

About ORKG Ask
Report issue
Statistics
Contact

Legal

Terms of use
Data protection (sheet)
Imprint
Accessibility
License

Technical

We
open source
System status
Changelog
Frontend: v1.41.0
Backend: v1.13.4

We use cookies to provide a better user experience.

Data Protection

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

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

Publication date

January 1972

Publisher

Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service],

Abstract

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

Extracted data

Related items

Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body /

Sleeman, William C.
Robins, A. Warner.
Langley Research Center.

Cover title.Includes bibliographical references (p. 18).Mode of access: Internet

Finite element analysis and computer graphics visualization of flow around pitching and plunging airfoils /

Bratanow, Theodore.
Ecer, Akin.
Langley Research Center.
University of Wisconsin--Milwaukee.

January 1973

"Prepared by University of Wisconsin-Milwaukee ... for Langley Research Center."Cover title.Bibliogr...

Numerical methods for the design and analysis of wings at supersonic speeds /

Carlson, Harry W.
Miller, David S.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 29-30).Mode ...

Application of numerical optimization to the design of low-speed airfoils /

Hicks, R. M. (Raymond Morton), 1932-
Vanderplaats, Garret N.
Ames Research Center.

January 1975

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 11).Mode of acc...

Experimental and theoretical low-speed aerodynamic characteristics of the NACA 65₁-213, a = 0.50 airfoil /

Beasley, William D.
McGhee, William D.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ...

Investigation of the static lift capability of a low-aspect-ratio wing operating in a powered ground-effect mode /

Huffman, Jarrett K.
Jackson, Charlie M.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 3).Mode of a...

Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model /

Applin, Zachary T.
Gentry, Garl L.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 21.Mode of access: Internet

Automated procedure for design of wing structures to satisfy strength and flutter requirements /

Haftka, Raphael T.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 22-24.Mode of access: Internet

Maneuver and buffet characteristics of fighter aircraft /

Ray, Edward J.
Carmichael, Julian G.
McKinney, Linwood W.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 16.Mode of access: Internet

Low-speed wind-tunnel investigation of flight dynamic characteristics of an advanced turboprop business/commuter aircraft configuration /

Coe, Paul L.
Owens, D. B. (Donald Bruce), 1922-
Turner, Steven G. (Steven George)
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 12.Mode of access: Internet

Analysis of transonic flow about lifting wing-body configurations /

Barnwell, Richard W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

High-speed flow past wings /

Nørstrud, Helge, 1934-
Langley Research Center.
Lockheed-Georgia Company.

January 1973

"Prepared by Lockheed-Georgia Company ... for Langley Research Center."Cover title.Bibliography: p. ...

Experimental low-speed and calculated high-speed aerodynamic characteristics of a hypersonic research airplane concept having a 65 ̊swept delta wing /

Penland, Jim A.
Howard, Floyd G.
Creel, Theodore R.
Langley Research Center.

January 1974

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

Hypersonic aerodynamics and entry-maneuver--aerothermodynamic interactions for two lifting entry vehicles /

Arrington, James P.
Woods, William C.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 12.Mode of access: Internet

Lowspeed wind-tunnel investigation of a semispan STOL jet transport wing-body with an upper-surface blown jet flap /

Phelps, Arthur R.
Henderson, Robert L.
Letko, William.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 12.Mode of access: Internet

Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body /

Sleeman, William C.
Robins, A. Warner.
Langley Research Center.

Cover title.Includes bibliographical references (p. 18).Mode of access: Internet

Finite element analysis and computer graphics visualization of flow around pitching and plunging airfoils /

Bratanow, Theodore.
Ecer, Akin.
Langley Research Center.
University of Wisconsin--Milwaukee.

January 1973

"Prepared by University of Wisconsin-Milwaukee ... for Langley Research Center."Cover title.Bibliogr...

Numerical methods for the design and analysis of wings at supersonic speeds /

Carlson, Harry W.
Miller, David S.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 29-30).Mode ...

Application of numerical optimization to the design of low-speed airfoils /

Hicks, R. M. (Raymond Morton), 1932-
Vanderplaats, Garret N.
Ames Research Center.

January 1975

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 11).Mode of acc...

Experimental and theoretical low-speed aerodynamic characteristics of the NACA 65₁-213, a = 0.50 airfoil /

Beasley, William D.
McGhee, William D.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ...

Investigation of the static lift capability of a low-aspect-ratio wing operating in a powered ground-effect mode /

Huffman, Jarrett K.
Jackson, Charlie M.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 3).Mode of a...

Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model /

Applin, Zachary T.
Gentry, Garl L.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 21.Mode of access: Internet

Automated procedure for design of wing structures to satisfy strength and flutter requirements /

Haftka, Raphael T.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 22-24.Mode of access: Internet

Maneuver and buffet characteristics of fighter aircraft /

Ray, Edward J.
Carmichael, Julian G.
McKinney, Linwood W.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 16.Mode of access: Internet

Low-speed wind-tunnel investigation of flight dynamic characteristics of an advanced turboprop business/commuter aircraft configuration /

Coe, Paul L.
Owens, D. B. (Donald Bruce), 1922-
Turner, Steven G. (Steven George)
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 12.Mode of access: Internet

Analysis of transonic flow about lifting wing-body configurations /

Barnwell, Richard W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

High-speed flow past wings /

Nørstrud, Helge, 1934-
Langley Research Center.
Lockheed-Georgia Company.

January 1973

"Prepared by Lockheed-Georgia Company ... for Langley Research Center."Cover title.Bibliography: p. ...

Experimental low-speed and calculated high-speed aerodynamic characteristics of a hypersonic research airplane concept having a 65 ̊swept delta wing /

Penland, Jim A.
Howard, Floyd G.
Creel, Theodore R.
Langley Research Center.

January 1974

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

Hypersonic aerodynamics and entry-maneuver--aerothermodynamic interactions for two lifting entry vehicles /

Arrington, James P.
Woods, William C.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 12.Mode of access: Internet

Lowspeed wind-tunnel investigation of a semispan STOL jet transport wing-body with an upper-surface blown jet flap /

Phelps, Arthur R.
Henderson, Robert L.
Letko, William.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 12.Mode of access: Internet

Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body /

Sleeman, William C.
Robins, A. Warner.
Langley Research Center.

Cover title.Includes bibliographical references (p. 18).Mode of access: Internet

Finite element analysis and computer graphics visualization of flow around pitching and plunging airfoils /

Bratanow, Theodore.
Ecer, Akin.
Langley Research Center.
University of Wisconsin--Milwaukee.

January 1973

"Prepared by University of Wisconsin-Milwaukee ... for Langley Research Center."Cover title.Bibliogr...

Numerical methods for the design and analysis of wings at supersonic speeds /

Carlson, Harry W.
Miller, David S.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 29-30).Mode ...