Accession Number : ADA116261

Title :   Shock-Free Configurations in Two- and Three- Dimensional Transonic Flow,

Corporate Author : ARIZONA UNIV TUCSON ENGINEERING EXPERIMENT STATION

Personal Author(s) : Seebass,A Robert

PDF Url : ADA116261

Report Date : May 1981

Pagination or Media Count : 22

Abstract : An indirect method for finding shock-free airfoils and a nearly direct method for finding shock-free airfoils and wing are discussed. While the mathematics of both procedures is emphasized, illustrative practical results are given. (Author)

Descriptors :   *Airfoils, *Wings, *Aerodynamic configurations, *Shock waves, *Transonic flow, Fluid dynamics, Shape, Mathematical models, Algorithms, Computerized simulation, Applied mathematics, Two dimensional, Three dimensional, Jet aircraft, Turbojet engines

Subject Categories : Aircraft
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE