Optimum element density studies for finite-element thermal analysis of hypersonic aircraft structures /

A study for development of aerothermodynamic test model materials and fabrication technique /

Dean, W. G.
Connor, L. E.
Langley Research Center.
Lockheed Missiles and Space Company.

January 1972

"Prepared by Lockheed Missiles & Space Company ... for Langley Research Center."Cover title.Bibliogr...

Optimum design of insulated tension members subjected to aerodynamic heating /

Davidson, John R., NASA researcher.
Langley Research Center.

January 1959

"NASA TN D-117.""Langley Research Center, Langley Field, Va.""December 1959."Title from cover.Includ...

Aerodynamic testing technique for twin-fuselage models at hypersonic speeds /

Ashby, George C.
Langley Research Center.

January 1975

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

Real-time aerodynamic heating and surface temperature calculations for hypersonic flight simulation /

Quinn, Robert D.
Gong, Leslie.
Dryden Flight Research Facility.

January 1990

Prepared at the Dryden Flight Research Facility.Bibliography: p. 10.Mode of access: Internet

Determination of the effects of heating on modal characteristics of an aluminum plate with application to hypersonic vehicles /

Snyder, H. Todd.
Kehoe, M. W.
Dryden Flight Research Facility.

January 1991

Prepared at Dryden Flight Research Facility.Bibliography: p. 7.Mode of access: Internet

Development of an integrated aeroservoelastic analysis program and correlation with test data /

Gupta, Kajal K.
Voelker, L. S.
Brenner, M. J.
Dryden Flight Research Facility.

January 1991

Prepared at the Dryden Flight Research Facility.Bibliography: p. 39.Mode of access: Internet

Studies of optimum body shapes at hypersonic speeds /

Stivers, Louis S., Jr.
Spender, Bernard, Jr.
Langley Research Center.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Prepared at Ames Research Center and Langley Research Center."N67-40121."Includes bibliographical re...

An analytical study of hydrogen cooled panels for application to hypersonic aircraft /

Flieder, W. G.
Langley Research Center.
Garrett Corporation.
United States. National Aeronautics and Space Administration.

January 1971

Prepared by The Garrett Corporation for Langley Research Center.N71-22625.Includes bibliographical r...

Thermal-structural combined loads design criteria study /

Deriugin, V.
Langley Research Center.
Boeing Company.

January 1972

"Prepared by the Boeing Company ... for Langley Research Center."Cover title.Bibliography: p. 273-27...

Compressive buckling analysis of hat-stiffened panel /

Ko, William L.
Jackson, Raymond H.
Dryden Flight Research Facility.

January 1991

Prepared at Dryden Flight Research Facility.Bibliography: p. 9.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 ...

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

Propulsion system/flight control integration and optimization : flight evaluation and technology transition /

Burcham, Frank W.
Myers, Lawrence P.
Gilyard, Glenn B.
Dryden Flight Research Facility.

January 1990

Prepared at Dryden Flight Research Facility.Bibliography: p. 9-10.Mode of access: Internet

Thermal dynamic modeling study /

Ojalvo, I. U.
Langley Research Center.
Grumman Aerospace Corporation.

January 1972

"Prepared by Grumman Aerospace Corporation ... for Langley Research Center."Cover title.Bibliography...

Thermal and structural tests of René 41 honeycomb integral-tank concept for future space transportation systems /

Shideler, John L.
Dryden Flight Research Facility.

January 1992

Prepared at Dryden Flight Research Facility.Includes bibliographical references (p. 13-14).Mode of a...

A study for development of aerothermodynamic test model materials and fabrication technique /

Dean, W. G.
Connor, L. E.
Langley Research Center.
Lockheed Missiles and Space Company.

January 1972

"Prepared by Lockheed Missiles & Space Company ... for Langley Research Center."Cover title.Bibliogr...

Optimum design of insulated tension members subjected to aerodynamic heating /

Davidson, John R., NASA researcher.
Langley Research Center.

January 1959

"NASA TN D-117.""Langley Research Center, Langley Field, Va.""December 1959."Title from cover.Includ...

Aerodynamic testing technique for twin-fuselage models at hypersonic speeds /

Ashby, George C.
Langley Research Center.

January 1975

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

Real-time aerodynamic heating and surface temperature calculations for hypersonic flight simulation /

Quinn, Robert D.
Gong, Leslie.
Dryden Flight Research Facility.

January 1990

Prepared at the Dryden Flight Research Facility.Bibliography: p. 10.Mode of access: Internet

Determination of the effects of heating on modal characteristics of an aluminum plate with application to hypersonic vehicles /

Snyder, H. Todd.
Kehoe, M. W.
Dryden Flight Research Facility.

January 1991

Prepared at Dryden Flight Research Facility.Bibliography: p. 7.Mode of access: Internet

Development of an integrated aeroservoelastic analysis program and correlation with test data /

Gupta, Kajal K.
Voelker, L. S.
Brenner, M. J.
Dryden Flight Research Facility.

January 1991

Prepared at the Dryden Flight Research Facility.Bibliography: p. 39.Mode of access: Internet

Studies of optimum body shapes at hypersonic speeds /

Stivers, Louis S., Jr.
Spender, Bernard, Jr.
Langley Research Center.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Prepared at Ames Research Center and Langley Research Center."N67-40121."Includes bibliographical re...

An analytical study of hydrogen cooled panels for application to hypersonic aircraft /

Flieder, W. G.
Langley Research Center.
Garrett Corporation.
United States. National Aeronautics and Space Administration.

January 1971

Prepared by The Garrett Corporation for Langley Research Center.N71-22625.Includes bibliographical r...

Thermal-structural combined loads design criteria study /

Deriugin, V.
Langley Research Center.
Boeing Company.

January 1972

"Prepared by the Boeing Company ... for Langley Research Center."Cover title.Bibliography: p. 273-27...

Compressive buckling analysis of hat-stiffened panel /

Ko, William L.
Jackson, Raymond H.
Dryden Flight Research Facility.

January 1991

Prepared at Dryden Flight Research Facility.Bibliography: p. 9.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 ...

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

Propulsion system/flight control integration and optimization : flight evaluation and technology transition /

Burcham, Frank W.
Myers, Lawrence P.
Gilyard, Glenn B.
Dryden Flight Research Facility.

January 1990

Prepared at Dryden Flight Research Facility.Bibliography: p. 9-10.Mode of access: Internet

Thermal dynamic modeling study /

Ojalvo, I. U.
Langley Research Center.
Grumman Aerospace Corporation.

January 1972

"Prepared by Grumman Aerospace Corporation ... for Langley Research Center."Cover title.Bibliography...

Thermal and structural tests of René 41 honeycomb integral-tank concept for future space transportation systems /

Shideler, John L.
Dryden Flight Research Facility.

January 1992

Prepared at Dryden Flight Research Facility.Includes bibliographical references (p. 13-14).Mode of a...

A study for development of aerothermodynamic test model materials and fabrication technique /

Dean, W. G.
Connor, L. E.
Langley Research Center.
Lockheed Missiles and Space Company.

January 1972

"Prepared by Lockheed Missiles & Space Company ... for Langley Research Center."Cover title.Bibliogr...

Optimum design of insulated tension members subjected to aerodynamic heating /

Davidson, John R., NASA researcher.
Langley Research Center.

January 1959

"NASA TN D-117.""Langley Research Center, Langley Field, Va.""December 1959."Title from cover.Includ...

Aerodynamic testing technique for twin-fuselage models at hypersonic speeds /

Ashby, George C.
Langley Research Center.

January 1975

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

Optimum element density studies for finite-element thermal analysis of hypersonic aircraft structures /

Abstract

Extracted data

Optimum element density studies for finite-element thermal analysis of hypersonic aircraft structures /

Abstract

Extracted data

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