A hybrid airfoil design method to simulate full-scale ice accretion throughout a given Cl-range

A hybrid airfoil design method to simulate full-scale ice accretion throughout a given Cl-range

著者名:

Saeed, Farooq ( University of Illinois at Urbana-Champaign )
Selig, Michael S.
Bragg, Michael B.

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:

1997

発行年:

1997

通号:

97-0054

ペーパー番号:

97-0054

開始ページ:

1

終了ページ:

10

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:	ZA00050850
シリーズID:	PA00000138
会議名:	Aerospace Sciences Meeting and Exhibit
回次:	35th
会議開催地:	Reno, NV
会議開催年:	1997.01.06-1997.01.10
論文注記:	35th Aerospace Sciences Meeting & Exhibit, January 6-10, 1997/Reno, NV

類似資料:

1 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	7 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
2 テクニカルペーパー A design procedure for subscale airfoils wth full-scale leading-edges for ice accretion testing Saeed, Farooq, Seilig, Michael S., Bragg, Michael B. American Institute of Aeronautics and Astronautics	8 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
3 テクニカルペーパー Hybrid Wing Design to Match Full- Scale Wing Ice Accretion Uppuluri, S., Selig, M.S. American Institute of Aeronautics and Astronautics	9 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
4 テクニカルペーパー A new class of airfoils with slot-suction Saeed, Farooq, Selig, Michael S. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Collection Efficiency and Ice Accretion Characteristics of Two Full Scale and One 1/4 Scale Business Jet Horizontal Tails Bidwell, Colin S., Papadakis, Michael Society of Automotive Engineers
5 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	11 テクニカルペーパー Effect of High-Fidelity Ice Accretion Simulations on the Performance of a Full-Scale Airfoil Model A. Broeren, M. Bragg, H. Addy, Jr., S. Lee, F. Moens, D. Guffond ONERA American Institute of Aeronautics and Astronautics
6 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	12 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

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