HIGH REYNOLDS NUMBER SUBSONIC AERODYNAMICS.

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.

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1970
Accession Number
AD0710329

Entities

People

  • Rolland A. Willaume

Organizations

  • AGARD

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamics
  • Aircrafts
  • Computers
  • Engine Components
  • Engines
  • Fluid Dynamics
  • Fluid Mechanics
  • Mechanics
  • Physics
  • Reynolds Number
  • Transport Ships
  • Vehicles

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Fluid Mechanics and Fluid Dynamics.