Vortex Flow Behavior Over Slender Delta Wing Configurations: Experimental Studies, Numerical and Analytical Solutions

by Xing Z. Huang and N. G. Verhaagen

Discusses the behavior of vortices over sharp and highly swept wing configurations used for military aircraft. This title pays attention to the effects of critical flow phenomenon such as vortex breakdown occurring at high angles of attack or high angular rates. It gives a validation and verification of the analytical and CFD solutions.

• Format: Hardcover
• Language: English
• ISBN: 1402093322
• ISBN13: 9781402093326
• Release Date: November 2008
• Publisher: Springer
• Length: 516 Pages