The Next Generation of High-Speed Dynamic Stability Wind Tunnel Testing (Invited)

The Next Generation of High-Speed Dynamic Stability Wind Tunnel Testing (Invited)

著者名:

D. Tomek ( NASA Langley Research Center, Hampton, VA )
W. Sewall
S. Mason ( Jacobs Sverdrup, Inc., Hampton, VA )
B. Szchur ( Sierra Lobo, Inc., Hampton, VA )

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : AIAA Aerodynamic Measurement Technology and Ground Test Conference

シリーズ巻号:

2006

発行年:

2006

通号:

2006-3148

ペーパー番号:

AIAA Paper 2006-3148

出版情報:

Reston, Va: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200611 [CD-ROM 2006 Disc 11]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00047233
シリーズID:	PA00000165
会議名:	AIAA Aerodynamic Measurement Technology and Ground Testing Conference
回次:	25th
会議開催地:	San Francisco, California
会議開催年:	2006.06.05-2006.06.08

類似資料:

1 テクニカルペーパー WIND TUNNEL RESULTS FOR A HIGH-SPEED, NATURAL LAMINAR-FLOW AIRFOIL DESIGNED FOR GENERAL AVIATION AIRCRAFT Sewall, William G. et al. National Aeronautics and Space Administration	7 テクニカルペーパー Wind Tunnel Experiments and Navier-Stokes Computations of a High-Lift Military Airfoil Dodbele, S. S., Hobbs, C. R., Kern, S. B., Ghee, T. A., Hall, D. R., Ely, W. L. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Development of Dynamic Stability Derivatives of an Airplane from Static Wind Tunnel Tests Chang, B., Cho, S., Cho,T., Lim, K., Hwang,S. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Dynamic Response Tests of Inertial and Optical Wind-Tunnel Model Attitude Measurement Devices Buehrle, R.D., Young, C.P., Jr., Burner, A.W., Tripp, J.S., Tcheng, P., Finley, T.D., Popernack, T.G., Jr. National Aeronautics and Space Adminstration
3 テクニカルペーパー Low Speed Wind Tunnel Testing of a Laser Propelled Vehicle Panetta, A. D., Nagamatsu, H. T., Myrabo, L. N., Minucci, M. A. S., Mead, F. B., Jr. Society of Automotive Engineers	9 テクニカルペーパー Wind tunnel experiments and Navier-Stokes computations of a high-lift military airfoil Dodbele, S.S., Hobbs, C.R., Kern, S.B., Ghee, T.A., Hall, D.R., Ely, W.L. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Wind Tunnel Test of an RPV with Shape-Change Effector and Sensor Arrays Raney, D., Cabell, R., Sloan, A., Hautamaki, B., Barnwell, W., Lion, S. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Low Speed Wind Tunnel Buffet Testing on the F/A-22 Anderson, W., Patel, S., Black, C. American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Subsonic and Transonic Dynamic Stability Characteristics of the X-33 Tomek, D., Boyden, R. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Dynamic Testing of a Subscale Sunshield for the Next Generation Space Telescope (NGST) Lienard,S., Johnston,J., Ross,B., Smith,J. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Plans and Status of Wind-Tunnel Testing Employing an Aeroservoelastic Semispan Model B. Perry, W. Silva, J. Florance, C. Wieseman, A. Pototzky, M. Sanetrik, R. Scott, D. Keller, S. Cole, D. Coulson American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Dynamic Wind-Tunnel Testing of a Sub-Scale Iced Business Jet S. Lee, B. Barnhart, T. Ratvasky, E. Dickes, M. Thacker American Institute of Aeronautics and Astronautics

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