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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)
Microform図書
1997<YCA-NAS 1.26:204315>
National Diet Library
  • Subject HeadingWing 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)
Microform図書
1996<YCA-NAS 1.26:203275>
National Diet Library
  • Subject Heading...configurations Body-wing configurations Design analysis Potential fl...

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)
Microform図書
1999<YCA-NAS 1.15:209534>
National Diet Library
  • Subject HeadingAerodynamic characteristics Body-wing configurations Nacelles Sonic booms Wings A...

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)
Microform図書
1996<YCA-NAS 1.26:206493>
National Diet Library
  • Subject Heading...Potential flow Body-wing configurations Configuration interaction Co...

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)
Microform図書
1996<YCA-NAS 1.15:207291>
National Diet Library
  • Subject HeadingBody-wing configurations Aeroelasticity Parallel comp...

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)
Microform図書
1999<YCA-NAS 1.60:209541>
National Diet Library
  • Subject Heading...ngle of attack Body-wing configurations Navier-Stokes equation Reyno...

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)
Microform図書
1997<YCA-NAS 1.60:3673>
National Diet Library
  • Subject Heading...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)
Microform図書
1996<YCA-NAS 1.26:203587>
National Diet Library
  • Subject Heading...haracteristics Body-wing configurations Navier-Stokes equation Finit...

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)
Microform図書
1989<YCA-NAS 1.26:4243>
National Diet Library
  • Subject Heading...ms (Computers) Body-wing configurations Computational geometry Compu...

Application of the wake integral method to CFD data

Application of the wake integral method to CFD data
Digital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
Other Libraries in Japan
  • Subject Heading...fluid dynamics body-wing configuration rectangular wing

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