Automated preliminary design of simplified wing structures to satisfy strength and flutter requirements /

An exploratory study of a parawing as a high-lift device for aircraft /

Naeseth, Rodger L.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mod...

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...

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

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

Aerodynamic-center considerations of wings and wing-body combinations /

Lamar, John E.
Alford, William J.
United States. National Aeronautics and Space Administration.

Cover title."October 1966."Includes bibliographical references.Mode of access: Internet

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

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...

Summary of flutter experiences as a guide to the preliminary design of lifting surfaces on missiles /

Martin, Dennis J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1951

"November 9, 1951."Includes bibliographical references (p. 12).Mode of access: Internet

Transonic and supersonic flutter trend investigation of a variable-sweep wing /

Stonesifer, John C.
Goetz, Robert C.
Langley Research Center.

January 1961

"October 1961."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Flutter analysis of swept-wing subsonic aircraft with parameter studies of composite wings /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 93).Mode of ...

Potential structural materials and design concepts for light aircraft /

Pazmany, Ladislao.
San Diego Aircraft Engineering, Inc.
NASA Headquarters Mission Analysis Division.
United States. National Aeronautics and Space Administration.

January 1969

"March 1969."Includes bibliographical references."Prepared under contract no.Mode of access: Interne...

Design techniques for small scientific satellite structures /

Madey, J. M.
Baumann, R. C.
United States. National Aeronautics and Space Administration.
Goddard Space Flight Center.

Prepared at Goddard Space Flight Center."July 1969 "--Cover.Includes bibliographical references (p. ...

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 ...

Aerodynamic data on large semispan tilting wing with 0.5-diameter chord, single-slotted flap, and single propeller 0.08 chord below wing /

Fink, Marvin P.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 12).Mode of access: Internet

Investigation of wing flutter at transonic speeds for six systematically varied wing plan forms /

Jones, George W.
DuBose, Hugh C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"August 13, 1953."Includes bibliographical references (p. 15).Mode of access: Internet

An exploratory study of a parawing as a high-lift device for aircraft /

Naeseth, Rodger L.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mod...

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...

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

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

Aerodynamic-center considerations of wings and wing-body combinations /

Lamar, John E.
Alford, William J.
United States. National Aeronautics and Space Administration.

Cover title."October 1966."Includes bibliographical references.Mode of access: Internet

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

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...

Summary of flutter experiences as a guide to the preliminary design of lifting surfaces on missiles /

Martin, Dennis J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1951

"November 9, 1951."Includes bibliographical references (p. 12).Mode of access: Internet

Transonic and supersonic flutter trend investigation of a variable-sweep wing /

Stonesifer, John C.
Goetz, Robert C.
Langley Research Center.

January 1961

"October 1961."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Flutter analysis of swept-wing subsonic aircraft with parameter studies of composite wings /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 93).Mode of ...

Potential structural materials and design concepts for light aircraft /

Pazmany, Ladislao.
San Diego Aircraft Engineering, Inc.
NASA Headquarters Mission Analysis Division.
United States. National Aeronautics and Space Administration.

January 1969

"March 1969."Includes bibliographical references."Prepared under contract no.Mode of access: Interne...

Design techniques for small scientific satellite structures /

Madey, J. M.
Baumann, R. C.
United States. National Aeronautics and Space Administration.
Goddard Space Flight Center.

Prepared at Goddard Space Flight Center."July 1969 "--Cover.Includes bibliographical references (p. ...

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 ...

Aerodynamic data on large semispan tilting wing with 0.5-diameter chord, single-slotted flap, and single propeller 0.08 chord below wing /

Fink, Marvin P.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 12).Mode of access: Internet

Investigation of wing flutter at transonic speeds for six systematically varied wing plan forms /

Jones, George W.
DuBose, Hugh C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"August 13, 1953."Includes bibliographical references (p. 15).Mode of access: Internet

An exploratory study of a parawing as a high-lift device for aircraft /

Naeseth, Rodger L.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mod...

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...

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

Automated preliminary design of simplified wing structures to satisfy strength and flutter requirements /

Abstract

Extracted data

Automated preliminary design of simplified wing structures to satisfy strength and flutter requirements /

Abstract

Extracted data

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