Accession Number : AD0850647

Title :   Demonstration of a Supersonic Box Method for Unsteady Aerodynamics of Nonplanar Wings. Part I. General Applications.

Descriptive Note : Technical rept. Mar 67-Sep 68,

Corporate Author : AIR FORCE FLIGHT DYNAMICS LAB WRIGHT-PATTERSON AFB OH

Personal Author(s) : Olsen, James J.

Report Date : FEB 1969

Pagination or Media Count : 78

Abstract : The report presents and interprets the calculations of the unsteady aerodynamic prediction method known as the 'Nonplanar Mach Box' method. It contains examples of data input and output for the associated computer program and explains the program's interpretation of the user's modal data. Also included are summaries of convergence properties, comparison with exact linearized theory, and a brief outline of the calculations for the Advisory Group for Aeronautical Research and Development (AGARD) planforms. (Author)

Descriptors :   (*SWEPTBACK WINGS, AERODYNAMIC CHARACTERISTICS), SUPERSONIC AIRCRAFT, DELTA WINGS, LIFT, DATA PROCESSING, THEORY, COMPUTER PROGRAMMING.

Subject Categories : Aircraft
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE