Calibration of the Test Section Mach Number in the JAXA 2m x 2m Transonic Wind Tunnel

Calibration of the Test Section Mach Number in the JAXA 2m x 2m Transonic Wind Tunnel

著者名:

M. Kohzai ( Japan Aerospace Exploration Agency, Chofu-shi, Tokyo, Japan )
M. Ueno
T. Shiohara
N. Sudani

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:

2008

発行年:

2008

通号:

2008-0848

ペーパー番号:

AIAA Paper 2008-0848

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200801 [CD-ROM 2008 Disc 1]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00049519
シリーズID:	PA00000138
会議名:	AIAA Aerospace Sciences Meeting and Exhibit
回次:	46th
会議開催地:	Reno, Nevada
会議開催年:	2008.01.07-2008.01.10
論文注記:	46th AIAA Aerospace Sciences Meeting and Exhibit, 7-10 January 2008, Reno, Nevada

類似資料:

1 テクニカルペーパー Flow Angularity Measurement of JAXA 2m × 2m Transonic Wind Tunnel M. Ueno, N. Sudani American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Evaluation of NACA0012 Airfoil Test Results in the NAL Two-Dimensional Transonic Wind Tunnel* SUDANI, Norikazu, KANDA, Hiroshi, SATO, Mamoru, MIWA, Hitoshi, MATSUNO, Kenichi, TAKANASHI, Susumu National Aeronautics and Space Adminstration
2 テクニカルペーパー Flow Qualities of JAXA Hypersonic Wind Tunnel Facilities M. Watari, N. Hirabayashi, T. Koyama, S. Nagai, S. Tsuda, H. Sekine, T. Yamazaki, K. Nakakita American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Exploitation by Airbus of High Reynolds Number Test Capabilities in the European Transonic Wind Tunnel White, P., Gibson,T. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel Schairer, Edward T., Lee, George, Mcdevitt, T. Kevin National Aeronautics and Space Adminstration	9 テクニカルペーパー Methods to Measure Acoustic Sources in a Closed Wind Tunnel Test Section Yamazaki, N., Nagakura, K., Ikeda, M., Sagawa, A. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー New Dynamic Stability Equipment for Transonic Wind Tunnel Testing at NAL Ueno,Makoto, Miwa,Hitoshi American Institute of Aeronautics and Astronautics	10 テクニカルペーパー EMPTY TEST SECTION STREAMLINING OF THE TRANSONIC SELF-STREAMLINING WIND TUNNEL FITTED WITH NEW MALLS Lewis, M. C. National Aeronautics and Space Administration
5 テクニカルペーパー WIND TUNNEL TESTS ON THE H3P78, POWER LAW, ELLIPTIC SECTION FLARED PROJECTILE FROM MACH 2.5 TO 4.0 Orchard,D.M., Fournier,E.Y., Dupuis,A., Edwards,J.A. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Design and Aerodynamic Calibration of the New AEDC Hypervelocity Wind Tunnel No. 9 Mach 8 Nozzle Norris, J., Lafferty, J., Smith, M., Collier, A., Hand, T. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Design of deep acoustic lining for the 40- by 80- Foot Wind Tunnel test section Soderman, Paul T., Schmitz, Fredric H., Allen, Christopher S., Jaeger, Stephen M., Sacco, Joe N., Hayes, Julie A. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Assessment of Wind Tunnel and CFD Transonic Base Pressure Using Flight Data M. Ueno, Y. Yamamoto, M. Yanagihara, M. Leplat, J. Oswald American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12