A Three-dimensional Non-reflecting Boundary Condition Treatment for Steady-state Flow Simulations

A Three-dimensional Non-reflecting Boundary Condition Treatment for Steady-state Flow Simulations

著者名:

J. Anker ( University of Stuttgart, Stuttgart, Germany )
B. Schrader
U. Seybold
J. Mayer
M. Casey

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

シリーズ巻号:

2006

発行年:

2006

通号:

2006-1275

ペーパー番号:

AIAA Paper 2006-1275

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200601 [CD-ROM 2006 Disc 1]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00047216
シリーズID:	PA00000138
会議名:	AIAA Aerospace Sciences Meeting and Exhibit
回次:	44th
会議開催地:	Reno, Nevada
会議開催年:	2006.01.09-2009.01.12

類似資料:

1 テクニカルペーパー A Preconditioned Solution Scheme for the Simulation of Turbomachinery Flow at Arbitrary Mach Numbers Anker, J., Mayer, J. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Three-dimensional effects on shock wave reflections in steady flows Sudani, N., Sato, M., Watanabe, M., Noda, J., Tate, A., Karasawa, T. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー A FAR-FIELD NON-REFLECTING BOUNDARY CONDITION FOR TWO-DIMENSIONAL WAKE FLOWS Danowitz, Jeffrey S., Abarbanel, Saul A., Turkel, Eli National Aeronautics and Space Adminstration	8 テクニカルペーパー EULER ANALYSIS OF THE THREE DIMENSIONAL FLOW FIELD OF A HIGH-SPEED PROPELLER: BOUNDARY CONDITION EFFECTS Nallasamy, M. National Aeronautics and Space Administration
3 テクニカルペーパー Steady and unsteady three dimensional flow field downstream of an embedded stator in a multistage axial flow compressor - Part 2: Composite flow field Suryavamshi, N., Lakshminarayana, B., Prato, J. The American Society of Mechanical Engineers	9 テクニカルペーパー Convergence acceleration for simulation of steady-state compressible flows using high-order schemes Iacono, Francesca, May, Georg American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Steady and unsteady three-dimensional flow field downstream of an embedded stator in a multistage axial flow compressor - Part 1: Unsteady velocity field Prato, J., Lakshminarayana, B., Suryavamshi, N. The American Society of Mechanical Engineers	10 テクニカルペーパー Approximate unsteady non-reflecting boundary conditions for the three-dimensional Euler equations Hoying, D.A. American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Steady and unsteady three dimensional flow field downstream of an embedded stator in a multistage axial flow compressor - Part 3: Deterministic stress and … Suryavamshi, N., Lakshminarayana, B., Prato, J. The American Society of Mechanical Engineers	11 テクニカルペーパー Three-dimensional Euler solutions for axisymmetric and non-axisymmetric advanced propeller flows Boyle, F.J., Flaherty, M.P.O., Eaton, J.A. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Three-Dimensional Effects on Shock Wave Reflections in Steady Flows Sudani, N., Sato, M., Watanabe, M., Noda, J., Tate, A., Karasawa, T. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Three-Dimensional Euler Solutions for Axisymmetric and Non-Axisymmetric Advanced Propeller Flows Boyle, F. J., Flaherty, M. P. O, Eaton, J. A. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12