Investigations on Shock Control Bumps for Infinite Swept Wings

Investigations on Shock Control Bumps for Infinite Swept Wings

著者名:

Kutzbach, M. ( University of Stuttgart, Stuttgart, Germany )
Lutz, T.
Wagner, S.

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : AIAA Flow Control Conference

シリーズ巻号:

2nd

発行年:

2004

通号:

2004-2702

ペーパー番号:

AIAA-2004-2702

出版情報:

[Reston, Va.]: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200409 [CD-ROM 2004 Disc 9]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001605
シリーズID:	PA00000172
会議名:	AIAA Flow Control Conference
回次:	2nd
会議開催地:	Portland, Oregon
会議開催年:	2004.06.28-2004.07.01

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1 テクニカルペーパー Numerical Optimization of Finite Shock Control Bumps M. Paetzold, T. Lutz, E. Kramer, S. Wagner American Institute of Aeronautics and Astronautics	7 テクニカルペーパー ANALYSIS OF TRANSITIONAL SEPARATION BUBBLES ON INFINITE SWEPT WINGS Davis, R.L. National Aeronautics and Space Administration
2 テクニカルペーパー Shock / Boundary-Layer Interaction Control Using Three-Dimensional Bumps for Transonic Wings H. Ogawa, H. Babinsky, M. Pätzold, T. Lutz American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Supersonic Laminar Flow Control on Swept Wings Using Distributed Roughness. Saric, W.S., Reed, H. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Numerical and Experimental Validation of Three-Dimensional Shock Control Bumps B. König, M. Pätzold, T. Lutz, E. Krämer, H. Rosemann, K. Richter, H. Uhlemann American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Application of Variable Leading-Edge Roughness for Transition Control on Swept Wings White, E.B., Saric, W.S. American Institute of Aeronautics and Astronautics
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5 テクニカルペーパー Numerical/experimental investigation of 3-D swept fin shock interactions Wright, M.J., Nowak, R.J., Berry, S.A., Glass, C.E., Candler, G.V. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Investigation of Transonic Flow over a Bump: Base Flow and Control G. Barakos, J. Huang, E. Benard, R. Yapalparvi, S. Raghunathan American Institute of Aeronautics and Astronautics
6 テクニカルペーパー A REVISED THEORY FOR THE FLOW OVER INFINITE SWEPT WINGS Nixon,David American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Adjoint-Based Optimisation of a Blended Wing Body Aircraft with Shock Control Bumps N. Qin, S. Wong, A. Le Moigne American Institute of Aeronautics and Astronautics

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