Accession Number : ADA302456
Title : Viscous Effects On Complex Configurations. Software User's Manual.
Descriptive Note : Final rept. Sep 92-Aug 95,
Corporate Author : MCDONNELL DOUGLAS AEROSPACE ST LOUIS MO
Personal Author(s) : Burns, K. A. ; Deters, K. J. ; Haley, C. P. ; Kihlken, T. A.
PDF Url : ADA302456
Report Date : AUG 1995
Pagination or Media Count : 259
Abstract : The Viscous Effects On Complex Configurations (VECC) program was a three task effort to improve preliminary aerodynamic prediction and analysis on high speed, arbitrary-shaped configurations. The first task was to incorporate a Newtonian streamline tracing code, 'QUADSTREAM', into a Graphical User Interface (GUl) system. The second task consisted of upgrades to the Supersonic-Hypersonic Arbitrary Body Program (SHABP). The third task, Pre-/Post-Processing, encompassed the development of the geometry modeling/display module, SHABP pre-processor, and the line plotting program. The improvements to SHABP included: level 2 viscous analysis (including aeroheating), shock shape/flowfield analysis, control deflections, and trimmed aerodynamic predictions. The VECC program is documented in two reports, (1) the program final report, WL-TR-95-3059, (2) the software user's manual, WL-Th-95-3060. (AN)
Descriptors : *SOFTWARE ENGINEERING, *VISCOUS FLOW, *AERODYNAMICS, DATA BASES, COMPUTER PROGRAM DOCUMENTATION, MATHEMATICAL MODELS, USER MANUALS, PREDICTIONS, SHOCK WAVES, DEFLECTION, INPUT OUTPUT PROCESSING, BOUNDARY LAYER, FLOW FIELDS, HYDRODYNAMIC CODES, COMPUTER GRAPHICS, SUBROUTINES, COMPUTER FILES, INVISCID FLOW, VISCOSITY, AERODYNAMIC HEATING, WING BODY CONFIGURATIONS, PRESSURE DISTRIBUTION, SKIN FRICTION, HYPERSONIC FLOW, STREAMLINE SHAPE.
Subject Categories : Aerodynamics
Computer Programming and Software
Distribution Statement : APPROVED FOR PUBLIC RELEASE