Analytic Drag Prediction for Cambered Wings with Partial Leading Edge Suction
Author:
- 1 January 2009
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 46 (1) , 312-319
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Unified Approximation for Nonparabolic Drag PolarsJournal of Aircraft, 2007
- Analytic prediction of lift for delta wings with partial leading-edge thrustJournal of Aircraft, 1994
- Drag of wings with cambered airfoils and partial leading-edge suctionJournal of Aircraft, 1983
- Studies of Leading-Edge Thrust PhenomenaJournal of Aircraft, 1980