A Hybrid Approach to Inverse Design of Complex Aerodynamic Systems

A Hybrid Approach to Inverse Design of Complex Aerodynamic Systems

著者名:

Gopalarathnam, Ashok ( Department of Mechanical and Aerospace Engineering North Carolina State University )
Selig, Michael S.

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:

2000

発行年:

2000

通号:

2000-0784

ペーパー番号:

00-0784

開始ページ:

1

終了ページ:

12

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:	ZA00050874
シリーズID:	PA00000138
会議名:	AIAA Aerospaces Science Meeting and Exhibit
回次:	38th
会議開催地:	Reno, NV
会議開催年:	2000.01.10-2000.01.13
論文注記:	38th AIAA Aerospace Sciences Meeting January 10-13, 2000/Reno, NV

類似資料:

1 テクニカルペーパー A hybrid method for multiple inverse wing design Gopalarathnam, Ashok, Selig, Michael S. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Design of Low Reynolds Number Airfoils with Trips Gopalarathnam,Ashok, Broughton,Benjamin A., McGranahan,Bryan D., Selig,Michael S. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー A Hybrid Method for Multipoint Inverse Wing Design Gopalarathnam, Ashok, Selig, Michael S. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー A Hybrid Inverse Design Method for Axisymmetric Bodies in Incompressible Flow Broughton, B., Selig, M. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー A multipoint inverse method for multi-element airfoil design Gopalarathnam, Ashok, Selig, Michael S. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー A hybrid airfoil design method to simulate full-scale ice accretion throughout a given Cl-range Saeed, Farooq, Selig, Michael S., Bragg, Michael B. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Low speed NLF airfoils: a case study in inverse airfoil design Gopalarathnam, Ashok, Selig, Michael S. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Post-Stall Aerodynamic Modeling and Gain-Scheduled Control Design Wu, F., Gopalarathnam, A., Kim, S. American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Low Speed NLF Airfoils: A Case Study in Inverse Airfoil Design Gopalarathnam, Ashok, Selig, Michael S. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー An Angle of Attack Correction Scheme for the Design of Low Aspect Ratio Wings With Endplates Soso, Michael, Selig, Michael S. Society of Automotive Engineering, Inc.
6 テクニカルペーパー Design of high-lift airfoils for low aspect ratio wings with endplates Gopalarathnam, Ashok, Selig, Michael S., Hsu, Frank American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Experimental validation of the hybrid airfoil design procedure for full-scale ice accretion simulation Saeed, Farooq, Selig, Michael S., Bragg, Michael B., Addy, Harold E., Jr. American Institute of Aeronautics and Astronautics

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