Accession Number : AD0740124

Title :   Investigation of Aerodynamic Analysis Problems in Transonic Maneuvering. Volume II. Airfoil Analysis Computer Program.

Descriptive Note : Final rept. Jun 70-Aug 71,

Corporate Author : DOUGLAS AIRCRAFT CO LONG BEACH CALIF

Personal Author(s) : Gentry,Arvel E.

Report Date : SEP 1971

Pagination or Media Count : 313

Abstract : The report describes a computer program designed to facilitate the analysis of mono- and multi-element airfoils at subsonic flight conditions with attached flow. This program is a consolidation of several existing computer programs so that they are compatible, have standard interfaces, and operate together as one very large program. This program includes a potential flow analysis, supercritical pressure calculations, and boundary layer calculations using either a finite-difference method or an integral method. Application studies using this program are described in Volume 1 of this report. (Author)

Descriptors :   (*TRANSONIC CHARACTERISTICS, *COMPUTER PROGRAMS), (*TRANSONIC AIRFOILS, NUMERICAL ANALYSIS), SUBSONIC CHARACTERISTICS, PRESSURE, BOUNDARY LAYER, BUFFETING

Subject Categories : Aerodynamics
      Computer Programming and Software
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE