Accession Number:

AD0639289

Title:

HIGH LIFT SURFACE DESIGN PROCEDURES. EXPERIMENTAL VERIFICATION. VOLUME II. THEORETICAL DESIGN AND ANALYSIS.

Descriptive Note:

Corporate Author:

NORAIR DIV NORTHROP CORP HAWTHORNE CALIF

Report Date:

1966-05-01

Pagination or Media Count:

126.0

Abstract:

The development of four wings which were designed to have specific aerodynamic requirements is described. The wings designed were a high lift wing, a low lift or cruise wing, both of which were smooth, and two flapped wings which were approximations of the smooth wings.

Subject Categories:

  • Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE