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Aerodynamic shape optimization for supersonic aircraft AIAA-2002-2838

Aerodynamic shape optimization for supersonic aircraft AIAA-2002-2838
Paper規格・テクニカルリポート類
Reuther, James2002<M-AIAA-2002-2838>
National Diet Library

Crew transfer vehicle trajectory optimization AIAA-2001-2885

Crew transfer vehicle trajectory optimization AIAA-2001-2885
Paper規格・テクニカルリポート類
Saunders, David, Allen, Gary, Jr, Gage, Peter, Reuther, James2001<M-AIAA-2001-2885>
National Diet Library

Low speed aerodynamics and landing characteristics of sharp-class crew transfer vehicle concepts AIAA-2001-2888

Low speed aerodynamics and landing characteristics of sharp-class crew transfer vehicle concepts AIAA-2001-2888
Paper規格・テクニカルリポート類
Smith, Stephen, Reuther, James, Kinney, David, Saunders, David2001<M-AIAA-2001-2888>
National Diet Library

A reusable space vehicle design study exploring sharp leading edges AIAA-2001-2884

A reusable space vehicle design study exploring sharp leading edges AIAA-2001-2884
Paper規格・テクニカルリポート類
Reuther, James, Kinney, David, Smith, Stephen, Kontinos, Dean, Gage, Peter, Saunders, David2001<M-AIAA-2001-2884>
National Diet Library

Constrained multipoint aerodynamic shape optimization using an adjoint formulation and parallel computers [microform] / James Reuther ... [et al.]

Constrained multipoint aerodynamic shape optimization using an adjoint formulation and parallel computers [microform] / James Reuther ... [et al.]
Microform図書
1997<YCA-NAS 1.26:204488>
National Diet Library
  • Author HeadingReuther, James United States. National Aeron...

An efficient multiblock method for aerodynamic analysis and design on distributed memory systems [microform] : to be presented at the AIAA 13th Computational Fluid Dynamics Conference, June 1997 / James Reuther ... [et al.] ([NASA contractor report] ; NASA-CR-204485) (RIACS technical report ; 97.05)

An efficient multiblock method for aerodynamic analysis and design on distributed memory systems [microform] : to be presented at the AIAA 13th Computational Fluid Dynamics Conference, June 1997 / James Reuther ... [et al.] ([NASA contractor report] ; NASA-CR-204485) (RIACS technical report ; 97.05)
Microform図書
1997<YCA-NAS 1.26:204485>
National Diet Library
  • Author HeadingReuther, James Research Institute for Advanc...

Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on parallel computers [microform] / James Reuther ... [et al.] ([NASA contractor report] ; NASA-CR-202390) (RIACS technical report ; 96.17)

Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on parallel computers [microform] / James Reuther ... [et al.] ([NASA contractor report] ; NASA-CR-202390) (RIACS technical report ; 96.17)
Microform図書
1996<YCA-NAS 1.26:203273>
National Diet Library
  • Author HeadingReuther, James Research Institute for Advanc...

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
  • Author HeadingReuther, James Research Institute for Advanc...

A coupled aero-structural optimization method for complete aircraft configurations AIAA-99-0187

A coupled aero-structural optimization method for complete aircraft configurations AIAA-99-0187
Paper規格・テクニカルリポート類
Reuther, James J, Alonso, Juan J, Martins, Joaquim R. R. A, Smith, Stephen C1999<M-AIAA-99-0187>
National Diet Library

The design of the Canyon Flyer, an airplane for Mars exploration AIAA-2000-0514

The design of the Canyon Flyer, an airplane for Mars exploration AIAA-2000-0514
Paper規格・テクニカルリポート類
Smith, Stephen C, Hahn, Andrew S, Johnson, Wayne R, Kinney, David J, Pollitt, Julie A, Reuther, James J2000<M-AIAA-2000-0514>
National Diet Library

Aerodynamic shape optimization techniques based on control theory AIAA-98-2538

Aerodynamic shape optimization techniques based on control theory AIAA-98-2538
Paper規格・テクニカルリポート類
Jameson, Antony, Alonso, Juan J, Reuther, James J, Martinelli, Luigi, Vassberg, John C1998<M-AIAA-98-2538>
National Diet Library

Business jet wing design using aerodynamic shape optimization AIAA-96-0554

Business jet wing design using aerodynamic shape optimization AIAA-96-0554
Paper規格・テクニカルリポート類
Gallman, John W, Reuther, James J, Pfeiffer, Neal J, Forrest, William C, Bernstorf, David J1996<M-AIAA-96-0554>
National Diet Library

A coupled aero-structural optimization method for complete aircraft configurations

A coupled aero-structural optimization method for complete aircraft configurations
Digital文書・図像類
Reuther, James J., Alonso, Juan J., Martins, Joaquim R. R. A., Smith, Stephen C.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.133-152
Other Libraries in Japan
  • Author HeadingReuther, James J. Alonso, Juan J. Martins, J...

EFFICIENT MULTIBLOCK METHOD FOR AERODYNAMIC ANALYSIS AND DESIGN ON DISTRIBUTED MEMORY SYSTEMS (NASA ; NASA-CR-204485)

EFFICIENT MULTIBLOCK METHOD FOR AERODYNAMIC ANALYSIS AND DESIGN ON DISTRIBUTED MEMORY SYSTEMS (NASA ; NASA-CR-204485)
Paper図書
REUTHER,JAMES RESEARCH INST. FOR ADVANCED COMPUTER SCIENCENational Aeronautics and Space Administration(National Aeronautics and Space Administration)1997.
Other Libraries in Japan

CONSTRAINED MULTIPOINT AERODYNAMIC SHAPE OPTIMIZATION USING AN ADJOINT FORMULATION AND PARALLEL (NASA ; NASA-CR-204488)

CONSTRAINED MULTIPOINT AERODYNAMIC SHAPE OPTIMIZATION USING AN ADJOINT FORMULATION AND PARALLEL (NASA ; NASA-CR-204488)
Paper図書
REUTHER, JAMES RESEARCH INST. FOR ADVANCED COMPUTER SOLENCENational Aeronautics and Space Administration(National Aeronautics and Space Administration)1997.
Other Libraries in Japan
  • Author HeadingREUTHER, JAMES RESEARCH INST. FOR ADVANCED C...

AERODYNAMIC SHAPE OPTIMIZATION OF COMPLEX AIRCRAFT CONFIGURATIONS VIA AN ADJOINT FORMULATION (NASA ; NASA-CR-203275)

AERODYNAMIC SHAPE OPTIMIZATION OF COMPLEX AIRCRAFT CONFIGURATIONS VIA AN ADJOINT FORMULATION (NASA ; NASA-CR-203275)
Paper図書
REUTHER,JAMES RESEARCH INST. FOR ADVANCED COMPUTER SCIENCENational Aeronautics and Space Administration(National Aeronautics and Space Administration)1996.
Other Libraries in Japan

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