Some recent applications of high-lift computational methods at Boeing
Author:
Affiliation:
1. Boeing Commercial Airplane Company, Seattle, Washington
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.44824
Reference9 articles.
1. 2Goldhammer, M.I. "A Lifting Surface Theory for the Analysis of Nonplanar Lifting Systems," AIAA Paper 76-16, Jan.1976.
2. 3Henderson, M.L. "Two-Dimensional Separated Wake Modeling and its Use to Predict Maximum Section Lift Coefficient," AIAA Paper 78-156, Jan.1978.
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1. Calculation of flow over multielement airfoils at high lift;Journal of Aircraft;1987-08
2. A method for predicting low-speed aerodynamic characteristics of transport aircraft;Journal of Aircraft;1984-03
3. A numerical procedure to predict the effects of Reynolds number and trip strip variation on three-dimensional wing lift and pitching moment;22nd Aerospace Sciences Meeting;1984-01-09
4. The impact of computational aerodynamics on aircraft design;10th Atmospheric Flight Mechanics Conference;1983-08-15
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