A REVISED THEORY FOR THE FLOW OVER INFINITE SWEPT WINGS | 東京工業大学附属図書館文献データベース

Blank Cover Image

A REVISED THEORY FOR THE FLOW OVER INFINITE SWEPT WINGS

Author(s):: Nixon,David ( Los Altos )
Publication title:: AIAA paper
Title of ser.:: AIAA Paper : Aerospace Sciences Meeting and Exhibit
Ser. no.:: 2001
Pub. Year:: 2001
No.:: 2001-0419
Paper no.:: AIAA-2001-0419
Page(from):: 1
Page(to):: 6
Pages:: 6
Pub. info.:: American Institute of Aeronautics and Astronautics
ISSN:: 01463705
Language:: English
Call no.:: A07400
Type:: Technical Paper

Details

TDL ID:	ZA00050880
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospace Sciences Meeting & Exhibit
Conf. info. (Number):	39th
Conf. info. (Venue):	Reno, Nevada
Conf. info. (Date):	2001.01.08-2001.01.11
Note for article:	39th AIAA Aerospace Sciences Meeting & Exhibit 8-11 January 2001/Reno, NV

Similar Items:

1 Technical Paper A Spectrally Accurate Boundary-Layer Code for Infinite Swept Wings Pruett, C. David National Aeronautics and Space Adminstration	7 Technical Paper A TRANSONIC INTERACTIVE BOUNDARY-LAYER THEORY FOR LAMINAR AND TURBULENT FLOW OVER SWEPT WINGS Final Report Woodson, Shawn H. et al. National Aeronautics and Space Administration
2 Technical Paper Conceptual design method for wings at transonic speeds Nixon, David American Institute of Aeronautics and Astronautics	8 Technical Paper Trailing-edge flows on highly-swept wings Shires, Andrew American Institute of Aeronautics and Astronautics
3 Technical Paper The Effect of Planform Curvature on the Compressible Flow over Wings Nixon, D. American Institute of Aeronautics and Astronautics	9 Technical Paper Aerodynamics and Flow Control Over Swept Wings and Wings with Diamond Planform J. Rullan, P. Vlachos, D. Telionis American Institute of Aeronautics and Astronautics
4 Technical Paper Investigations on Shock Control Bumps for Infinite Swept Wings Kutzbach, M., Lutz, T., Wagner, S. American Institute of Aeronautics and Astronautics	10 Technical Paper ALESEP. PART 2: A COMPUTER PROGRAM FOR THE ANALYSIS OF LEADING EDGE SEPARATION BUBBLES ON INFINITE SWEPT WINGS Davis, R.L. National Aeronautics and Space Administration
5 Technical Paper ANALYSIS OF TRANSITIONAL SEPARATION BUBBLES ON INFINITE SWEPT WINGS Davis, R.L. National Aeronautics and Space Administration	11 Technical Paper Simple Adaptive Planforms for Wings. Nixon, D. Society of Automotive Engineers
6 Technical Paper Observations on non-dissipative algorithms for transonic flow Nixon, David American Institute of Aeronautics and Astronautics	12 Technical Paper Experimental study of the flow around two scaled 3D swept wings Gooden, J.H.M., Gleyzes, C., Maciel, Y. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12