Grid generation by elliptic partial differential equations for a tri-element Augmentor-Wing airfoil-Reference-Cited by-同舟云学术

Grid generation by elliptic partial differential equations for a tri-element Augmentor-Wing airfoil

Published:1982-01 Issue: Volume:10-11 Page:653-665
ISSN:0096-3003
Container-title:Applied Mathematics and Computation
language:en
Short-container-title:Applied Mathematics and Computation

Author:

Sorenson Reese L.

Publisher

Elsevier BV

Subject

Applied Mathematics,Computational Mathematics

Reference16 articles.

1. A Flight Investigation of the STOL Characteristics of an Augmented Jet Flap STOL Research Aircraft;Quigley;NASA TM-X 62334,1974

2. Comparison of Model and Flight Test Data for an Augmentor-Wing STOL Research Aircraft;Whittley;AGARD Flight Mechanics Symposium,Valloire, France, June 9–12,1975

3. The Transonic Multi-Foil Augmentor-Wing;Farbridge;AIAA Paper 77-606,1977

4. Analysis of Results From Test of an Asymmetric High Speed Augmentor-Wing Model (WTCB) in the NAE Two-Dimensional High Reynolds Number Blowdown Tunnel;DHC-DIR 75-2,1975

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