Accession Number:

AD0766639

Title:

STOL Tactical Aircraft Investigation. Volume 2. Part 1. Aerodynamic Technology: Design Compendium, Vectored Thrust/Mechanical Flaps

Descriptive Note:

Final technical rept. 8 Jun 1971-8 Dec 1972

Corporate Author:

BOEING AEROSPACE CO SEATTLE WA

Report Date:

1973-05-01

Pagination or Media Count:

236.0

Abstract:

The report presents methods for predicting the performance determining aerodynamic characteristics and the stability derivatives of transport-type configurations employing the vectored-thrust mechanical-flap high-lift concept. These methods are suitable for preliminary design. They have been automated in a FORTRAN 4 computer program, for which a users manual and listing are included in this document.

Subject Categories:

  • VSTOL

Distribution Statement:

APPROVED FOR PUBLIC RELEASE