Accession Number : ADA333243
Title : Conceptual and Preliminary Level Modeling of Wings Using the Adaptive Modeling Language
Descriptive Note : Final rept. Sep 96-jun 97
Corporate Author : WRIGHT LAB WRIGHT-PATTERSON AFB OH FLIGHT DYNAMICS DIRECTORATE
Personal Author(s) : Bharatram, Geetha ; Zweber, Jeffrey V.
PDF Url : ADA333243
Report Date : JUN 1997
Pagination or Media Count : 32
Abstract : This memorandum demonstrates a methodology for an automated design process. The design process was developed in the Adaptive Modeling Language (AML). This effort concentrates on developing a system for linking conceptual level wing geometric parameters to a preliminary level finite element model. This environment allows for rapid changes in the geometric parameters of the wing planform (e.g., wing sweep, span, chord length, etc.) as well as the capability for updating internal substructure (i.e., number and placement of ribs, spars and stiffeners) in an integrated environment. In this effort, a fully associative geometric design model (developed in AML) is coupled with an aerospace structural optimization code, ASTROS.
Descriptors : *COMPUTER AIDED DESIGN, *SWEPT WINGS, *AIRCRAFT DESIGN, *OBJECT ORIENTED PROGRAMMING, INTEGRATED SYSTEMS, FINITE ELEMENT ANALYSIS, ADAPTIVE SYSTEMS, ASSOCIATIVE PROCESSING, KNOWLEDGE BASED SYSTEMS, AIRCRAFT MODELS, MACHINE CODING, PLANFORM.
Subject Categories : Aircraft
Computer Programming and Software
Distribution Statement : APPROVED FOR PUBLIC RELEASE