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Conceptual Design Shop: A Tool for Rapid Airframe Structural ModelingThis paper presents an innovative approach to rapidly generate finite element (FE) models of a complete airframe for a variety of airframe concepts. The current implementation of this software includes all airfoil surfaces and the fuselage, and is limited to FE modeling of low-wing designs with T-tails or twin tails. This tool, called the Conceptual Design Shop (CDS), was developed using the PATRAN command language (PCL) within the PATRAN finite element modeling software. CDS is an attempt to fill a gap in current finite element modeling software to automatically connect wings and tails to the fuselage in airframe models. The CDS software is demonstrated on two airframe designs: a generic transport aircraft and an advanced aircraft design with a boundary-layer ingestion engine.
Document ID
20180006181
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Mason, Brian H.
(NASA Langley Research Center Hampton, VA, United States)
Quinlan, Jesse R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
October 9, 2018
Publication Date
January 8, 2018
Subject Category
Computer Programming And Software
Report/Patent Number
NF1676L-27364
Report Number: NF1676L-27364
Meeting Information
Meeting: AIAA SciTech
Location: Kissimmee, FL
Country: United States
Start Date: January 8, 2018
End Date: January 12, 2018
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 081876.02.07.30.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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