Some aerodynamic principles for the design of swept wings
- 31 December 1962
- journal article
- review article
- Published by Elsevier in Progress in Aerospace Sciences
- Vol. 3, 1-83
- https://doi.org/10.1016/0376-0421(62)90016-7
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- The Design of Wing Plan Forms for Transonic SpeedsAeronautical Quarterly, 1961
- An Introduction to the Flow about Plane Swept-back Wings at Transonic SpeedsJournal of the Royal Aeronautical Society, 1960
- Wings with Minimum Drag Due to Lift in Supersonic FlowJournal of the Aerospace Sciences, 1960
- Wing Section Design for Swept-Back Wings at Transonic SpeedsJournal of the Royal Aeronautical Society, 1957
- Methods of Reducing the Transonic Drag of Swept - Back Wings at Zero LiftJournal of the Royal Aeronautical Society, 1957
- Tests of a Fairing to Reduce the Drag of a Supersonic Swept-Wing RootJournal of the Aeronautical Sciences, 1955
- The Distribution of Lift over the Surface of Swept WingsAeronautical Quarterly, 1953
- Slender-Body Theory-Review and ExtensionJournal of the Aeronautical Sciences, 1953
- The Minimum Drag of Thin Wings in Frictionless FlowJournal of the Aeronautical Sciences, 1951
- Notes on the Linear Theory of Incompressible Flow Round Symmetrical Swept-Back Wings at Zero LiftAeronautical Quarterly, 1949