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The radiated field generated by a monopole source in a short, rigid, rectangular duct [microform] : a thesis submitted to the Faculty of the School of Engineering and Applied Science of the George Washington University in partial satisfaction of the requirements for the degree of Master of Science / Barbara Anne Lakota (NASA/TM ; 1998-207543)

The radiated field generated by a monopole source in a short, rigid, rectangular duct [microform] : a thesis submitted to the Faculty of the School of Engineering and Applied Science of the George Washington University in partial satisfaction of the requirements for the degree of Master of Science / Barbara Anne Lakota (NASA/TM ; 1998-207543)
マイクロ図書
1998<YCA-NAS 1.15:207543>
国立国会図書館
  • 件名Ducts Monopoles Sound fields Singular integral equations Shape functions Boundary integral method

PROFILE [microform] : airfoil geometry manipulation and display : user's guide / Leslie Collins, David Saunders (NASA contractor report ; 177332)

PROFILE [microform] : airfoil geometry manipulation and display : user's guide / Leslie Collins, David Saunders (NASA contractor report ; 177332)
マイクロ図書
1997<YCA-NAS 1.26:177332>
国立国会図書館
  • 件名...ms (Computers) Shape functions Aerodynamics

Research on Analysis Techniques for Beam Structures Using Functionally Graded Materials by Means of Finite Element Method

Research on Analysis Techniques for Beam Structures Using Functionally Graded Materials by Means of Finite Element Method
デジタル博士論文障害者向け資料あり
TRINH,THANH,HUONG2017-03-25
インターネットで読める国立国会図書館全国の図書館
  • 件名...od of Analysis Shape Function

A novel shape parameterization approach [microform] / Jamshid A. Samareh (NASA/TM ; 1999-209116)

A novel shape parameterization approach [microform] / Jamshid A. Samareh (NASA/TM ; 1999-209116)
マイクロ図書
1999<YCA-NAS 1.15:209116>
国立国会図書館
  • 件名...element method Shape functions Structural analysis Computat...

Aerodynamic optimization of supersonic wing-nacelle configuration using an adjoint method with the unstructured-grid approach

Aerodynamic optimization of supersonic wing-nacelle configuration using an adjoint method with the unstructured-grid approach
デジタル文書・図像類
Kim, Hyoung-Jin, 大林, 茂, 中橋, 和博, Obayashi, Shigeru, Nakahashi, Kazuhiro航空宇宙技術研究所2000-12航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory49Tp.121-129
全国の図書館
  • 件名...od Hicks Henne shape function elliptic equation method sequ...
  • 一般注記...n. Hicks-Henne shape functions are adopted for the surface ...

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