Prediction of Superboom Problem Using Computational Solution of Nonlinear Tricomi Equation

Prediction of Superboom Problem Using Computational Solution of Nonlinear Tricomi Equation

著者名:

Kandil, O. ( Old Dominion University, Norfolk, VA )
Zheng, X.

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : AIAA Atmospheric Flight Mechanics Conference

シリーズ巻号:

2005

発行年:

2005

通号:

2005-6335

ペーパー番号:

AIAA Paper 2005-6335

出版情報:

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

ISSN:

10877215

言語:

英語

請求記号:

A07400/200516 [CD-ROM 2005 Disc 16]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001636
シリーズID:	PA00000162
会議名:	AIAA Atmospheric Flight Mechanics Conference and Exhibit
回次:	2005
会議開催地:	San Francisco, California
会議開催年:	2005.08.15-2005.08.18

類似資料:

1 テクニカルペーパー Parametric Investigation of Sonic Boom Focusing using Solution of Nonlinear Tricomi Equation O. Kandil, N. Khasdeo American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Sonic Boom Computations for Double-Cone Configuration Using CFL3D, FUN3D and Full-Potential Codes O. Kandil, I. Ozcer American Institute of Aeronautics and Astronautics
2 テクニカルペーパー COMPUTATIONAL TECHNIQUE FOR COMPRESSIBLE VORTEX FLOWS USING THE INTEGRAL EQUATION SOLUTION Kandil, Osaama A. National Aeronautics and Space Administration	8 テクニカルペーパー THE SOLUTION OF BOUNDARY LAYER PROBLEMS BY THE USE OF INTEGRAL EQUATIONS: POLL, D. National Aeronautics and Space Adminstration
3 テクニカルペーパー SOLUTIONS OF BOUNDARY VALUE PROBLEMS FOR THE TRICOMI-EQUATION. GROOTHUIZEN, R.J.P. National Aeronautics and Space Administration	9 テクニカルペーパー Prediction of Sonic Boom Signature Using Euler-Full Potential CFD with Grid Adaptation and Shock Fitting Kandil, O., Yang, Z., Bobbitt, P. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Development of Computational Sensing and Active Flow Control of Airfoils During Dynamic Stall Kandil, O., Gercek, E., Zheng, X., Luo,X. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Numerical solution of acoustic propagation problems using linearized Euler's equations Bailly, Christophe, Juve, Daniel American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Comparison of Full-Potential Propagation-Code Computations with the F-5E "Shaped Sonic Boom Experiment" Program Kandil, O., Ozcer, I., Zheng, X., Bobbitt, P. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Trailing-Edge Noise Prediction Using the Nonlinear Disturbance Equations J. Erwin, P. Morris, K. Brentner American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Multigrid, multiblock computation of incompressible flows using two-equation turbulent models Zheng, X., Liao, C., Liu, C., Sung, C.H., Huang, T.T. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー NUMERICAL SOLUTIONS OF ACOUSTIC WAVE PROPAGATION PROBLEMS USING EULER COMPUTATIONS Hariharan, S. I. National Aeronautics and Space Administration

1

2

3

4

5

6

7

8

9

10

11

12