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

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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 programs interpretation of the users 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

Author(s):
Olsen, James J.
Author Organization(s):
AIR FORCE FLIGHT DYNAMICS LAB WRIGHT-PATTERSON AFB OH
Descriptive Note:
Technical rept. Mar 67-Sep 68,
Pagination:
0078

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
AFFDL-TR-67-104-Pt-1
Task Number(s):
137003
Project Number(s):
AF-1370
 Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
(*SWEPTBACK WINGS, AERODYNAMIC CHARACTERISTICS), SUPERSONIC AIRCRAFT, DELTA WINGS, LIFT, DATA PROCESSING, THEORY, COMPUTER PROGRAMMING
Field(s)/Group(s):
Aircraft, Fluid Mechanics
Keyword(s):
COMPUTER ANALYSIS, RECTANGULAR WINGS, *SUPERSONIC MACH BOX METHOD, *UNSTEADY AERODYNAMICS
Report Date:
1969 Feb 01