Accession Number:

ADA951925

Title:

An Analysis of the Flow over Two 45 deg Swept-Back Wings at High Subsonic Speeds, and Comparison with Theory.

Descriptive Note:

Reports and memoranda,

Corporate Author:

AERONAUTICAL RESEARCH COUNCIL LONDON (ENGLAND)

Personal Author(s):

Report Date:

1961-01-01

Pagination or Media Count:

42.0

Abstract:

Subject Categories:

  • Aircraft
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE