A method to account for partial leading-edge suction and vortex flow for swept and delta wings at subsonic and supersonic speeds

Report (1994)

Authors

Faculty
Aerospace Engineering (Aerospace Engineering) (TU Delft)
Copyright: © 1994 Delft University of Technology
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Published Date

1994

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Source:

Delft University of Technology, Faculty of Aerospace Engineering, Report LR-779

Faculty

Aerospace Engineering

Files

LR-779.pdf
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