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An interactive user-friendly approach to surface-fitting three-dimensional geometriesA surface-fitting technique has been developed which addresses two problems with existing geometry packages: computer storage requirements and the time required of the user for the initial setup of the geometry model. Coordinates of cross sections are fit using segments of general conic sections. The next step is to blend the cross-sectional curve-fits in the longitudinal direction using general conics to fit specific meridional half-planes. Provisions are made to allow the fitting of fuselages and wings so that entire wing-body combinations may be modeled. This report includes the development of the technique along with a User's Guide for the various menus within the program. Results for the modeling of the Space Shuttle and a proposed Aeroassist Flight Experiment geometry are presented.
Document ID
19880010674
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cheatwood, F. Mcneil
(North Carolina State Univ. Raleigh, NC, United States)
Dejarnette, Fred R.
(North Carolina State Univ. Raleigh, NC, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1988
Subject Category
Numerical Analysis
Report/Patent Number
NASA-CR-4126
NAS 1.26:4126
Report Number: NASA-CR-4126
Report Number: NAS 1.26:4126
Accession Number
88N20058
Funding Number(s)
PROJECT: RTOP 506-40-11-01
CONTRACT_GRANT: NCC1-22
CONTRACT_GRANT: NCC1-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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