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検索結果 10 件

Wing weight optimization under aeroelastic loads subject to stress constraints [microform] / Rakesh K. Kapania ... [et al.] ([NASA contractor report] ; NASA CR-204315)

Wing weight optimization under aeroelastic loads subject to stress constraints [microform] / Rakesh K. Kapania ... [et al.] ([NASA contractor report] ; NASA CR-204315)
マイクロ図書
1997<YCA-NAS 1.26:204315>
国立国会図書館
  • 件名Wing loading Optimization Aeroelasticity Stress analysis Body-wing configurations

Aerodynamic shape optimization of complex aircraft configurations via an adjoint formulation [microform] / James Reuther ... [et al.] ([NASA contractor report] ; NASA-CR-203275) (RIACS technical report ; 96.02)

Aerodynamic shape optimization of complex aircraft configurations via an adjoint formulation [microform] / James Reuther ... [et al.] ([NASA contractor report] ; NASA-CR-203275) (RIACS technical report ; 96.02)
マイクロ図書
1996<YCA-NAS 1.26:203275>
国立国会図書館
  • 件名...configurations Body-wing configurations Design analysis Potential flo...

Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds [microform] / Robert J. Mack ([NASA technical memorandum] ; NASA/TM-1999-209534)

Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds [microform] / Robert J. Mack ([NASA technical memorandum] ; NASA/TM-1999-209534)
マイクロ図書
1999<YCA-NAS 1.15:209534>
国立国会図書館
  • 件名Aerodynamic characteristics Body-wing configurations Nacelles Sonic booms Wings Ae...

Study of the mutual interaction between a wing wake and an encountering airplane [microform] : NASA grant no. NAG1-1572, final report / by A.B. Walden, C.P. van Dam ([NASA contractor report] ; 206493)

Study of the mutual interaction between a wing wake and an encountering airplane [microform] : NASA grant no. NAG1-1572, final report / by A.B. Walden, C.P. van Dam ([NASA contractor report] ; 206493)
マイクロ図書
1996<YCA-NAS 1.26:206493>
国立国会図書館
  • 件名...Potential flow Body-wing configurations Configuration interaction Com...

Wing-body aeroelasticity on parallel computers [microform] / Chansup Byun and Guru P. Guruswamy ([NASA technical memorandum] ; 207291)

Wing-body aeroelasticity on parallel computers [microform] / Chansup Byun and Guru P. Guruswamy ([NASA technical memorandum] ; 207291)
マイクロ図書
1996<YCA-NAS 1.15:207291>
国立国会図書館
  • 件名Body-wing configurations Aeroelasticity Parallel compu...

Navier-Stokes simulation of several high-lift reference H configurations [microform] / Wendy B. Lessard (NASA/TP ; 1999-209541)

Navier-Stokes simulation of several high-lift reference H configurations [microform] / Wendy B. Lessard (NASA/TP ; 1999-209541)
マイクロ図書
1999<YCA-NAS 1.60:209541>
国立国会図書館
  • 件名...ngle of attack Body-wing configurations Navier-Stokes equation Reynol...

Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results [microform] / Jim A. Penland and Richard Hawkins (NASA technical paper ; 3673)

Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results [microform] / Jim A. Penland and Richard Hawkins (NASA technical paper ; 3673)
マイクロ図書
1997<YCA-NAS 1.60:3673>
国立国会図書館
  • 件名...fluid dynamics Body-wing configurations Aerodynamic drag Aerodynamic ...

Development of multiobjective optimization techniques for sonic boom minimization [microform] : final report on NASA Ames grant no. NCC2-5064, performance period--5/16/94-9/15/96 / principal investigators: Aditi Chattopadhyay and John Narayan Rajadas, Narayanan S. Pagaldipti ([NASA contractor report] ; NASA-CR-203587)

Development of multiobjective optimization techniques for sonic boom minimization [microform] : final report on NASA Ames grant no. NCC2-5064, performance period--5/16/94-9/15/96 / principal investigators: Aditi Chattopadhyay and John Narayan Rajadas, Narayanan S. Pagaldipti ([NASA contractor report] ; NASA-CR-203587)
マイクロ図書
1996<YCA-NAS 1.26:203587>
国立国会図書館
  • 件名...haracteristics Body-wing configurations Navier-Stokes equation Finite...

HOMAR:a computer code for generating homotopic grids using algebraic relations [microform] : users' manual / Anutosh Moitra (NASA contractor report ; 4243)

HOMAR:a computer code for generating homotopic grids using algebraic relations [microform] : users' manual / Anutosh Moitra (NASA contractor report ; 4243)
マイクロ図書
1989<YCA-NAS 1.26:4243>
国立国会図書館
  • 件名...ms (Computers) Body-wing configurations Computational geometry Comput...

Application of the wake integral method to CFD data

Application of the wake integral method to CFD data
デジタル文書・図像類
上野, 真, 赤塚, 純一, Ueno, Makoto, Akatsuka, Junichi宇宙航空研究開発機構2008-02-29宇宙航空研究開発機構研究開発報告 = JAXA Research and Development ReportJAXA-RR-07-030E
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