Conceptual design method for wings at transonic speeds

Conceptual design method for wings at transonic speeds

Author(s):: Nixon, David ( NWING Inc. )
Publication title:: A collection of technical papers : 15th AIAA Applied Aerodynamics Conference, June 23-25, 1997, Atlanta, GA
Title of ser.:: AIAA Paper : AIAA Applied Aerodynamics Conference
Ser. no.:: CP978
Pub. Year:: 1997
Vol.:: pt. 1
No.:: 97-2241
Paper no.:: AIAA-97-2241
Page(from):: 239
Page(to):: 246
Pub. info.:: Reston, VA: American Institute of Aeronautics and Astronautics
ISBN:: 9781563472329 [1563472325]
Language:: English
Call no.:: (pt.1)A07400/978-1,(pt.2)A07400/978-2
Type:: Technical Paper

Details

TDL ID:	ZA00001967
Series ID:	PA00000157
Conf. info. (Name):	AIAA Applied Aerodynamics Conference
Conf. info. (Number):	15th
Conf. info. (Venue):	Atlanta, GA
Conf. info. (Date):	1997.06.23-1997.06.25

Similar Items:

1 Technical Paper A universal indicial function for pressure prediction at transonic speeds Nixon, David American Institute of Aeronautics and Astronautics	7 Technical Paper APPLICATION OF TIME-LINEARIZED METHODS TO OSCILLATING WINGS IN TRANSONIC… HOUNJET, M.H.L. National Aeronautics and Space Administration
2 Technical Paper A Method for the Design of Transonic Flexible Wings Smith, Leigh Ann, Campbell, Richard L. National Aeronautics and Space Adminstration	8 Technical Paper Debris Signature Analysis(SM) : A Method for Assessing the Detrimental Effect of Specific Debris Contaminated Lubrication Environments Nixon, Harvey P., Cogdell, J. David Society of Automotive Engineers
3 Technical Paper A REVISED THEORY FOR THE FLOW OVER INFINITE SWEPT WINGS Nixon,David American Institute of Aeronautics and Astronautics	9 Technical Paper The Effect of Planform Curvature on the Compressible Flow over Wings Nixon, D. American Institute of Aeronautics and Astronautics
4 Technical Paper Observations on non-dissipative algorithms for transonic flow Nixon, David American Institute of Aeronautics and Astronautics	10 Technical Paper Conceptual design optimization of composite wings with aeroelasic and strength constraints Lillico, M., Butler, R., Holden, M. American Institute of Aeronautics and Astronautics
5 Technical Paper A METHOD OF ESTIMATING THE ONSET OF SHOCK INDUCED BUFFET Nixon,David American Institute of Aeronautics and Astronautics	11 Technical Paper A Conceptual Design Methodology for Predicting the Aerodynamics of Upper Surface Blowing on Airfoils and Wings Keen, E., Mason, W. American Institute of Aeronautics and Astronautics
6 Technical Paper Simple Adaptive Planforms for Wings. Nixon, D. Society of Automotive Engineers	12 Technical Paper Tip Extensions, Winglets, and C-wings: Conceptual Design and Optimization A. Ning, I. Kroo American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12