Aerodynamic Characteristics of Slender Delta Wing with Low Dorsal Fin

Aerodynamic Characteristics of Slender Delta Wing with Low Dorsal Fin

Author(s):

X. Meng ( Northwestern Polytechnical University, Xi'an, China (prc) )

C. Jia

Z. Qiao

C. Gao

S. Luo ( University of California, Irvine, Irvine, CA )

F. Liu

1 more

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2007

Pub. Year:

2007

No.:

2007-1272

Paper no.:

AIAA Paper 2007-1272

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200701 [CD-ROM 2007 Disc 1]

Type:

Technical Paper

Details

TDL ID:	ZA00050739
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	45th
Conf. info. (Venue):	Reno, Nevada
Conf. info. (Date):	2007.01.08-2007.01.11

Similar Items:

1 Technical Paper Flow Over Delta Wing with Low Dorsal Fin-PIV Study X. Meng, Z. Qiao, C. Gao, S. Luo, F. Liu American Institute of Aeronautics and Astronautics	7 Technical Paper Flow Control over a Conical Forebody Using Duty-cycled Plasma Actuators F. Liu, S. Luo, C. Gao, X. Meng, J. Hao, J. Wang, Z. Zhao American Institute of Aeronautics and Astronautics
2 Technical Paper Visualization of Vortex Flow over Delta Wing with Dorsal Fin Meng, X., Qiao, Z., Gao, C., Luo, S., Liu, F. American Institute of Aeronautics and Astronautics	8 Technical Paper Stability of Symmetric and Asymmetric Vortex Pairs Over Slender Conical Wing-Body Combinations Cai, J., Luo, S., Liu, F. American Institute of Aeronautics and Astronautics
3 Technical Paper Asymmetry Features Independent of Roll Angle for Slender Circular Cone X. Meng, Z. Qiao, C. Gao, S. Luo, F. Liu American Institute of Aeronautics and Astronautics	9 Technical Paper Stability of Symmetric and Asymmetric Vortex Pairs Over Slender Conical Wings and Bodies Cai, J., Luo, S., Liu, F. American Institute of Aeronautics and Astronautics
4 Technical Paper Pressure around a 20-degree Circular Cone at 35-degree Angle of Attack and Low Speed C. Jia, X. Meng, Z. Qiao, C. Gao, S. Luo, F. Liu American Institute of Aeronautics and Astronautics	10 Technical Paper Calculation of Airfoil Flutterby an Euler Method with Approximate Boundary Conditions Gao, C., Luo, S., Liu, F., Schuster, D. American Institute of Aeronautics and Astronautics
5 Technical Paper Development of Flow Asymmetry with Angle of Attack Over a 20-Degree Circular Cone at Low Speed X. Meng, C. Jia, Z. Qiao, C. Gao, s. Luo, F. Liu American Institute of Aeronautics and Astronautics	11 Technical Paper BUFFETING OF A FLEXIBLE FIN OVER A DELTA WING Lambert,C., Gursul,I. American Institute of Aeronautics and Astronautics
6 Technical Paper Reynolds Number Effects on Cone Forebody Side Force X. Meng, Z. Qiao, C. Gao, S. Luo, F. Liu American Institute of Aeronautics and Astronautics	12 Technical Paper Vortex Core and Its Effects on the Stability of Vortex Flow over Slender Conical Bodies Cai, J., Tsai, H., Luo, S., Liu, F. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12