Integrated Aero-Propulsive CFD Methodology for the Hyper-X Flight Experiment

Integrated Aero-Propulsive CFD Methodology for the Hyper-X Flight Experiment

著者名:

Cockrell Jr.,C.

掲載資料名:

A collection of technical papers : 18th AIAA Applied Aerodynamics Conference, Denver, Colorado 14-17 August 2000

シリーズ名:

AIAA Paper : AIAA Applied Aerodynamics Conference

シリーズ巻号:

2000

発行年:

2000

巻:

v. 1

通号:

2000-4010

ペーパー番号:

AIAA-2000-4010

開始ページ:

161

終了ページ:

170

総ページ数:

10

出版情報:

Reston, VA: American Institute of Aeronautics and Astronautics

ISBN:

9781563473807 [1563473801]

言語:

英語

請求記号:

A07400/003917

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00000075
シリーズID:	PA00000157
会議名:	AIAA Applied Aerodynamics Conference
回次:	18th
会議開催地:	Denver, CO
会議開催年:	2000.08.14-2000.08.17

類似資料:

1 テクニカルペーパー Aerodynamic Database Development for the Hyper-X Airframe Integrated Scramjet Propulsion Experiments Engelund,W., Holland,S., Cockrell Jr.,C., Bittner,R. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Uncertainty Methodology for In-Flight Thrust Determination Adams,G.R., Thompson Jr.,J.W., Abernethy,R.B., Biesiadny,T., Havey,C.T., Steurer,J.W., Ascough,J.C., Williams,D.D. "Society of Automotive Engineering, Inc."
2 テクニカルペーパー Verification of a CFD Procedure for Aerodynamic Database Development Using the Hyper-X Stack Configuration Parikh, P., Engelund, W., Armand, S., Bittner, R. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー On the CFD Support for the Hyper-X Aerodynamic Database Frendi, Abdelkader American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Wind tunnel testing, flight scaling and flight validation with Hyper-X McClinton, C.R., Voland, R.T., Holland, S.D., Engelund, W.C., White, J.T., Pahle, J.W. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー On the CFD support for the hyper-X aerodynamic database Frendi, Abdelkader American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Preliminary Study of Integrated Aero-Propulsive Performance of Vehicle with CFD and Experiments J. Le, W. Liu, W. He, Y. He, Z. Zheng American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Aeroheating Predictions for the X- 43 Cowl- Closed Configuration at Mach 7 and 10 Cockrell, C.E., Jr., Auslender, A.H., White, J.A., Dilley, A.D. American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Hyper-X wind tunnel program McClinton, C.R., Holland, S.D., Rock, K.E., Engelund, W.C., Voland, R.T., Huebner, L.D., Rogers, R.C. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Mars ascent vehicle flight analysis Desai, P.N., Braun, R.D., Engelund, W.C., Cheatwood, F.M., Kangas, J.A. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Prediction of Hyper-X Stage Separation Aerodynamics using CFD Buning,P., Wong,T.-C., Dilley,A., Pao,J. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー An overview of the on-orbit results from the ESEX flight experiment Bromaghim, D.R., LeDuc, J.R., Salasovich, R.M., Zimmerman, J.A., Matias, D.C., Sutton, A.M., Spanjers, G.G., Fife, J.M., … American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12