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
Distribution Statement : APPROVED FOR PUBLIC RELEASE