Accession Number : AD0710329

Title :   HIGH REYNOLDS NUMBER SUBSONIC AERODYNAMICS.

Descriptive Note : Lecture series,

Corporate Author : ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT PARIS (FRANCE)

Personal Author(s) : Willaume,Rolland A.

Report Date : 1970

Pagination or Media Count : 266

Abstract : Contents: Advantages and problems of large subsonic aircraft; Aeromechanics; Scaling effects on shock-induced separation; Scaling effects on drag prediction; High Reynolds number subsonic aerodynamics; Advanced computer technology in aerodynamics; Engine performance considerations for the large subsonic transport; The aerodynamics of engine component design problems associated with large subsonic aircraft.

Descriptors :   (*SUBSONIC CHARACTERISTICS, *SYMPOSIA), (*TRANSPORT AIRCRAFT, SUBSONIC CHARACTERISTICS), REYNOLDS NUMBER, AEROELASTICITY, SHOCK WAVES, FLOW SEPARATION, DRAG, AIRCRAFT ENGINES

Subject Categories : Aerodynamics
      Transport Aircraft
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE