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

Study of flutter related computational procedures for minimum weight structural sizing of advanced aircraft /

O'Connell, Robert F.
Radovcich, N. A., joint author.
Hassig, H. J., joint author.
Lockheed-California Company.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 115-117).Mode of access: Internet

Flight-path and airspeed control during landing approach for powered-lift aircraft /

Franklin, James A.
Innis, Robert C.
Ames Research Center.

January 1974

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 59-60).Mode of ...

On the use of thick-airfoil theory to design airfoil families in which thickness and lift are varied independently /

Barger, Raymond L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 6).Mode of a...

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

A computer program for the design and analysis of low-speed airfoils /

Eppler, Richard A.
Somers, Dan M.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

"August 1980"--Cover.Includes bibliographical reference (p. 126).Mode of access: Internet

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 ...

Analysis of a theoretically optimized transonic airfoil /

Lores, M. E.
Shrewsbury, George D., 1939-
Burdges, Kenneth P.
Ames Research Center.
Lockheed-Georgia Company.

January 1978

"Prepared [at Lockheed-Georgia Company] for Ames Research Center under Contract NAS2-8697.""November...

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...

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 ...

Numerical calculations of velocity and pressure distribution around oscillating airfoils /

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

January 1974

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

Natural laminar flow airfoil design considerations for winglets on low-speed airplanes /

Van Dam, C. P. (Cornelis P.), 1954-
Langley Research Center.
Vigyan Research Associates.

January 1984

"Prepared [at Vigyan Research Associates] for Langley Research Center under Contract NAS1-17797.""De...

Simplified lifting-surface theory for flaps on wings of low and moderate aspect ratios /

Wick, Bradford H.
Ames Research Center.

January 1975

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 7).Mode of acce...

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 airfoil design using cartesian coordinates /

Carlson, Leland A.
Texas A. and M. Research Foundation.
United States. National Aeronautics and Space Administration.

January 1976

Prepared by Texas A & M Research Foundation, College Station, Tex. for Langley Research Center.Cover...

A streamline curvature method for design of supercritical and subcritical airfoils /

Barger, Raymond L.
Brooks, Cuyler W.
Langley Research Center.

January 1974

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

Study of flutter related computational procedures for minimum weight structural sizing of advanced aircraft /

O'Connell, Robert F.
Radovcich, N. A., joint author.
Hassig, H. J., joint author.
Lockheed-California Company.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 115-117).Mode of access: Internet

Flight-path and airspeed control during landing approach for powered-lift aircraft /

Franklin, James A.
Innis, Robert C.
Ames Research Center.

January 1974

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 59-60).Mode of ...

On the use of thick-airfoil theory to design airfoil families in which thickness and lift are varied independently /

Barger, Raymond L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 6).Mode of a...

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

A computer program for the design and analysis of low-speed airfoils /

Eppler, Richard A.
Somers, Dan M.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

"August 1980"--Cover.Includes bibliographical reference (p. 126).Mode of access: Internet

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 ...

Analysis of a theoretically optimized transonic airfoil /

Lores, M. E.
Shrewsbury, George D., 1939-
Burdges, Kenneth P.
Ames Research Center.
Lockheed-Georgia Company.

January 1978

"Prepared [at Lockheed-Georgia Company] for Ames Research Center under Contract NAS2-8697.""November...

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...

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 ...

Numerical calculations of velocity and pressure distribution around oscillating airfoils /

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

January 1974

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

Natural laminar flow airfoil design considerations for winglets on low-speed airplanes /

Van Dam, C. P. (Cornelis P.), 1954-
Langley Research Center.
Vigyan Research Associates.

January 1984

"Prepared [at Vigyan Research Associates] for Langley Research Center under Contract NAS1-17797.""De...

Simplified lifting-surface theory for flaps on wings of low and moderate aspect ratios /

Wick, Bradford H.
Ames Research Center.

January 1975

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 7).Mode of acce...

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 airfoil design using cartesian coordinates /

Carlson, Leland A.
Texas A. and M. Research Foundation.
United States. National Aeronautics and Space Administration.

January 1976

Prepared by Texas A & M Research Foundation, College Station, Tex. for Langley Research Center.Cover...

A streamline curvature method for design of supercritical and subcritical airfoils /

Barger, Raymond L.
Brooks, Cuyler W.
Langley Research Center.

January 1974

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

Study of flutter related computational procedures for minimum weight structural sizing of advanced aircraft /

O'Connell, Robert F.
Radovcich, N. A., joint author.
Hassig, H. J., joint author.
Lockheed-California Company.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 115-117).Mode of access: Internet

Flight-path and airspeed control during landing approach for powered-lift aircraft /

Franklin, James A.
Innis, Robert C.
Ames Research Center.

January 1974

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 59-60).Mode of ...

On the use of thick-airfoil theory to design airfoil families in which thickness and lift are varied independently /

Barger, Raymond L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 6).Mode of a...

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

Abstract

Extracted data

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

Abstract

Extracted data

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