Variable-complexity response surface approximations for wing structural weight in HSCT design

Variable-complexity response surface approximations for wing structural weight in HSCT design

著者名:

Kaufman, M. ( Virginia Polytechnic Institute and State Univ. )

掲載資料名:

AIAA paper

シリーズ名:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

シリーズ巻号:

1996

発行年:

1996

通号:

96-0089

ペーパー番号:

96-0089

開始ページ:

1

終了ページ:

18

出版情報:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

言語:

英語

請求記号:

A07400

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00050843
シリーズID:	PA00000138
会議名:	Aerospace Sciences Meeting and Exhibit
回次:	34th
会議開催地:	Reno, NV
会議開催年:	1996.01.15-1996.01.18
論文注記:	34th Aerospace Sciences Meeting & Exhibit, January 15-18, 1996/Reno, NV

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1 テクニカルペーパー Developing customized wing weight function by structural optimization on parallel computers Balabanov, V., Kaufman, M., Giunta, A.A., Haftka, Raphael T., Grossman, B., Mason, W.H., Watson, L.T. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー HSCT Configuration Design Space Exploration Using Aerodynamic Response Surface Approximations Baker,C., Grossman,B., Haftka,R., Mason,W., Watson,L. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー HSCT configuration design using response surface approximations of supersonic euler aerodynamics Knill, D.L., Giunta, A.A., Baker, C.A., Grossman, B., Mason, W.H., Haftka, R.T., Watson, L.T. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Certification of a CFD code for high-speed civil transport design optimization Knill, D.L., Balabanov, V., Grossman, B., Mason, W.H., Haftka, R.T. American Institute of Aeronautics and Astronautics
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4 テクニカルペーパー Multifidelity Response Surface Model for HSCT Wing Bending Material Weight Balabanov,V., Haftka,R., Grossman,B., Mason,W., Watson,L. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー An MDO investigation of the impact of practical constraints on an HSCT configuration MacMillin, P.E., Golovidov, O., Mason, W.H., Grossman, B., Haftka, R.T. American Institute of Aeronautics and Astronautics
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6 テクニカルペーパー Getting the full benefits of CFD in conceptual design Mason, W.H., Knill, D.L., Giunta, A.A., Grossman, B., Watson, L.T., Haftka, R.T. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Response surface approximations for structural optimization Roux, W.J., Stander, Nielen, Haftka, R.T. American Institute of Aeronautics and Astronautics

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