Accession Number:

ADA951918

Title:

A Study of the Effect of Leading-Edge Modifications on the Flow over a 50-deg Sweptback Wing at Transonic Speeds,

Descriptive Note:

Corporate Author:

AERONAUTICAL RESEARCH COUNCIL LONDON (ENGLAND)

Report Date:

1962-01-01

Pagination or Media Count:

83.0

Abstract:

Subject Categories:

  • Aircraft
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE