Performance augmentation of a 60-degree delta aircraft configurationby spanwise blowing
- 1 November 1986
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 23 (11) , 801-807
- https://doi.org/10.2514/3.45384
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
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- Numerical calculation of nonlinear aerodynamics of wing-body configurationsAIAA Journal, 1983
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- A Conceptual Study of Leading-Edge-Vortex Enhancement by BlowingJournal of Aircraft, 1974
- Predictions of vortex-lift characteristics by a leading-edge suctionanalogyJournal of Aircraft, 1971
- Possible Types of Flow at Swept Leading EdgesAeronautical Quarterly, 1964