Development of panel methods for subsonic analysis and design /

A preliminary investigation of modified blunt 13° half-cone re-entry configurations at subsonic speeds /

Kenyon, George C.
Edwards, George G.
Ames Research Center.

January 1961

"March 1961."Cover title.Includes bibliographical references (p. 14).Mode of access: Internet

Supersonic aerodynamics of large-angle cones /

Campbell, James F.
Howell, Dorothy T.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."August 1968."Includes bibliographical references (p. 13).Mode of access: Internet

1981 current research on aviation weather (bibliography) /

Daniel, Joel.
Frost, Walter, 1935-
George C. Marshall Space Flight Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject Category 47."March 1982"--Cover.Includes bibliographies.Mode of access: Internet

Subsonic panel method for designing wing surfaces from pressure distribution /

Bristow, D. R.
Hawk, J. Dennis.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"July 1983"--Cover.Distributed to depository libraries in microfiche."McDonnell Aircraft Company."Bi...

Development of a three-dimensional supersonic inlet flow analysis /

Buggeln, R. C.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"January 1980"--Cover.Includes bibliographical references.Mode of access: Internet

Flightweight radiantly and actively cooled panel : thermal and structural performance /

Shore, Charles P.
Kelly, H. Neale.
Nowak, Robert J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"October 1982"--Cover.Includes bibliographical references.Mode of access: Internet

A method for determining surface pressures on blunt bodies of revolution at small angles of attack in supersonic flow /

Jackson, Charlie M.
Smith, Rudeen S.
Sawyer, Wallace C.
United States. National Aeronautics and Space Administration.

Cover title."November 1968."Includes bibliographical references.Mode of access: Internet

Aerothermal performance of a radiatively and actively cooled panel at Mach 6.6 /

Shore, Charles P.
Weinstein, Irving.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 34."December 1979"--Cover.Includes bibliographical references.Mode of access: Inter...

Atmospheric studies related to aerospace activities and remote sensing technology /

Sze, N. D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 46."March 1981"--Cover.Bibliography: p. 124-138.Mode of access: Internet

Design and fabrication of a stringer stiffened discrete tube actively cooled panel for a hypersonic aircraft /

Anthony, Frank M.
Helenbrook, Robert G.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 39."February 1981."Includes bibliographical references.Mode of access: Internet

Semianalytic modeling of aerodynamic shapes /

Barger, Raymond L.
Adams, Mary S.
Langley Research Center.

January 1985

Prepared at Langley Research Center."April 1985"--Cover.Includes bibliographical references (p. 6).M...

Static investigation of several jet deflectors for longitudinal control of an aircraft /

Valerino, Alfred S.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "June 7, 1955."Title from cover.Includes bibliographical references: p. 9.Mode of ac...

Design guide for pitch-up evaluation and investigation at high subsonic speeds of possible limitations due to wing-aspect-ratio variations /

Spreemann, Kenneth P.
United States. National Aeronautics and Space Administration.

"August 1959."Cover title.Includes bibliographical references (p. 14-16).Mode of access: Internet

Development of aerodynamic prediction methods for irregular planform wings /

Benepe, David B.
General Dynamics Corporation.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 02."February 1983"--Cover."General Dynamics."Includes bibliographical references.Mo...

Investigation of the low-subsonic aerodynamic characteristics of a model of a modified lenticular reentry configuration /

Ware, George M.
Langley Research Center.

January 1962

"December 1962."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

A preliminary investigation of modified blunt 13° half-cone re-entry configurations at subsonic speeds /

Kenyon, George C.
Edwards, George G.
Ames Research Center.

January 1961

"March 1961."Cover title.Includes bibliographical references (p. 14).Mode of access: Internet

Supersonic aerodynamics of large-angle cones /

Campbell, James F.
Howell, Dorothy T.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."August 1968."Includes bibliographical references (p. 13).Mode of access: Internet

1981 current research on aviation weather (bibliography) /

Daniel, Joel.
Frost, Walter, 1935-
George C. Marshall Space Flight Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject Category 47."March 1982"--Cover.Includes bibliographies.Mode of access: Internet

Subsonic panel method for designing wing surfaces from pressure distribution /

Bristow, D. R.
Hawk, J. Dennis.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"July 1983"--Cover.Distributed to depository libraries in microfiche."McDonnell Aircraft Company."Bi...

Development of a three-dimensional supersonic inlet flow analysis /

Buggeln, R. C.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"January 1980"--Cover.Includes bibliographical references.Mode of access: Internet

Flightweight radiantly and actively cooled panel : thermal and structural performance /

Shore, Charles P.
Kelly, H. Neale.
Nowak, Robert J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"October 1982"--Cover.Includes bibliographical references.Mode of access: Internet

A method for determining surface pressures on blunt bodies of revolution at small angles of attack in supersonic flow /

Jackson, Charlie M.
Smith, Rudeen S.
Sawyer, Wallace C.
United States. National Aeronautics and Space Administration.

Cover title."November 1968."Includes bibliographical references.Mode of access: Internet

Aerothermal performance of a radiatively and actively cooled panel at Mach 6.6 /

Shore, Charles P.
Weinstein, Irving.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 34."December 1979"--Cover.Includes bibliographical references.Mode of access: Inter...

Atmospheric studies related to aerospace activities and remote sensing technology /

Sze, N. D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 46."March 1981"--Cover.Bibliography: p. 124-138.Mode of access: Internet

Design and fabrication of a stringer stiffened discrete tube actively cooled panel for a hypersonic aircraft /

Anthony, Frank M.
Helenbrook, Robert G.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 39."February 1981."Includes bibliographical references.Mode of access: Internet

Semianalytic modeling of aerodynamic shapes /

Barger, Raymond L.
Adams, Mary S.
Langley Research Center.

January 1985

Prepared at Langley Research Center."April 1985"--Cover.Includes bibliographical references (p. 6).M...

Static investigation of several jet deflectors for longitudinal control of an aircraft /

Valerino, Alfred S.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "June 7, 1955."Title from cover.Includes bibliographical references: p. 9.Mode of ac...

Design guide for pitch-up evaluation and investigation at high subsonic speeds of possible limitations due to wing-aspect-ratio variations /

Spreemann, Kenneth P.
United States. National Aeronautics and Space Administration.

"August 1959."Cover title.Includes bibliographical references (p. 14-16).Mode of access: Internet

Development of aerodynamic prediction methods for irregular planform wings /

Benepe, David B.
General Dynamics Corporation.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 02."February 1983"--Cover."General Dynamics."Includes bibliographical references.Mo...

Investigation of the low-subsonic aerodynamic characteristics of a model of a modified lenticular reentry configuration /

Ware, George M.
Langley Research Center.

January 1962

"December 1962."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

A preliminary investigation of modified blunt 13° half-cone re-entry configurations at subsonic speeds /

Kenyon, George C.
Edwards, George G.
Ames Research Center.

January 1961

"March 1961."Cover title.Includes bibliographical references (p. 14).Mode of access: Internet

Supersonic aerodynamics of large-angle cones /

Campbell, James F.
Howell, Dorothy T.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."August 1968."Includes bibliographical references (p. 13).Mode of access: Internet

1981 current research on aviation weather (bibliography) /

Daniel, Joel.
Frost, Walter, 1935-
George C. Marshall Space Flight Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject Category 47."March 1982"--Cover.Includes bibliographies.Mode of access: Internet

Development of panel methods for subsonic analysis and design /

Abstract

Extracted data

Development of panel methods for subsonic analysis and design /

Abstract

Extracted data

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