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検索結果 5 件

Computation of hypersonic transitional flows by solving three-dimensional Burnett equations AIAA-98-1607

Computation of hypersonic transitional flows by solving three-dimensional Burnett equations AIAA-98-1607
紙規格・テクニカルリポート類
Deng, Zheng-Tao, Liaw, Goang-Shin1998<M-AIAA-98-1607>
国立国会図書館

Exhausted plume flow field prediction near the afterbody of hypersonic flight vehicles in high altitudes [microform] / Zheng-Tao Deng ... [et al.] (NASA-TM ; 111872)

Exhausted plume flow field prediction near the afterbody of hypersonic flight vehicles in high altitudes [microform] / Zheng-Tao Deng ... [et al.] (NASA-TM ; 111872)
マイクロ図書
1995<YCA-NAS 1.15:111872>
国立国会図書館
  • 著者標目Deng, Zheng-Tao United States. National Aeron...

Computation of low-density axisymmetric nozzle flow fields by solving burnett equations AIAA-95-2008

Computation of low-density axisymmetric nozzle flow fields by solving burnett equations AIAA-95-2008
紙規格・テクニカルリポート類
Deng, Zheng-Tao, Liaw, Goang-Shin, Chou, Lynn Chen1995<M-AIAA-95-2008>
国立国会図書館

Exhausted plume flow field prediction near the afterbody of hypersonic flight vehicles in high altitudes AIAA-95-6069

Exhausted plume flow field prediction near the afterbody of hypersonic flight vehicles in high altitudes AIAA-95-6069
紙規格・テクニカルリポート類
Deng, Zheng-Tao, Liaw, Goang-Shin, Chou, Lynn Chen, Mach, Kervyn D1995<M-AIAA-95-6069>
国立国会図書館

Numerical investigations of low-density nozzle flow by solving the Boltzmann equation AIAA-95-0627

Numerical investigations of low-density nozzle flow by solving the Boltzmann equation AIAA-95-0627
紙規格・テクニカルリポート類
Deng, Zheng-Tao, Liaw, Goang-Shin, Chou, Lynn Chen<M-AIAA-95-0627>
国立国会図書館

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