Blank Cover Image

Application of the vortex lattice CFD method to obtaining unsteady aerodynamic predictions about wing/fuselage/pylon/store configuration including store separation

著者名:
Kaykayoglu, C. Ruhi ( Istanbul University, Turkey )  
掲載資料名:
AIAA paper
シリーズ名:
AIAA Paper : Aerospace Sciences Meeting and Exhibit
シリーズ巻号:
1996
発行年:
1996
通号:
96-0168
ペーパー番号:
96-0168
開始ページ:
1
終了ページ:
11
出版情報:
American Institute of Aeronautics and Astronautics
ISSN:
01463705
言語:
英語
請求記号:
A07400
資料種別:
テクニカルペーパー

類似資料:

1 テクニカルペーパー Unsteady Aerodynamic Coefficients Obtained by a Compressible Vortex Lattice Method

F. Hernandes, P. Soviero

American Institute of Aeronautics and Astronautics
7 テクニカルペーパー UNSTEADY TRANSONIC FLOW CALCULATIONS FOR WING-FUSELAGE CONFIGURATIONS

Batina, J.T.

National Aeronautics and Space Administration
2 テクニカルペーパー Prediction of Store Trajectory Response to Unsteady Aerodynamic Loads

C. Nelson, A. Cain

American Institute of Aeronautics and Astronautics
8 テクニカルペーパー A System for Simulation of Store Separation Including Unsteady Effects

K. Roughen, X. Wang, M. Baker, O. Bendiksen

American Institute of Aeronautics and Astronautics
3 テクニカルペーパー PREDICTION OF LOADS ON WING/BODY/EXTERNAL STORE/FINS PYLON-CONFIGURATIONS AN TRANSONIC SPEEDS

Wang, Dieqian et al.

National Aeronautics and Space Administration
9 テクニカルペーパー AERODYNAMIC CHARACTERISTICS OF A HIGH-WING TRANSPORT CONFIGURATION WITH A OVER-THE-WING NACELLE-PYLON ARRANGEMENT

Henderson, W.P.

National Aeronautics and Space Administration
4 テクニカルペーパー Incorporation of CFD Generated Aerodynamic Data in Store Separation Predictions

Dunworth, K., Atkins, D., Lee, J.

American Institute of Aeronautics and Astronautics
10 テクニカルペーパー Unsteady Wing-Pylon-Nacelle Interference in Transonic Flow

G. Dietz, H. Mai, A. Schroeder, C. Klein, N. Moreaux, P. Leconte

American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Aerodynamic Design of Wing-Body-Nacelle-Pylon Configuration

Koc, S., Kim, H., Nakahashi, K.

American Institute of Aeronautics and Astronautics
11 テクニカルペーパー AEROELASTIC ANALYSIS OF AIRCRAFT: WING AND WING/FUSELAGE CONFIGURATIONS

Chen, H. H., Chang, K. C., Tzong, T., Cebeci, T.

National Aeronautics and Space Adminstration
6 テクニカルペーパー Analytical Sensitivity Analysis of an Unsteady Vortex Lattice Method for Flapping Wing Optimization

Stanford, Bret K., Beran, Philip S.

American Institute of Aeronautics and Astronautics
12 テクニカルペーパー Aeroelastic analysis of wing and wing/fuselage configurations

Chen, H.H., Chang, K.C., Tzong, T., Cebeci, T.

American Institute of Aeronautics and Astronautics
1
 
2
 
3
 
4
 
5
 
6
 
7
 
8
 
9
 
10
 
11
 
12