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User's guide for a computer program for calculating the zero-lift wave drag of complex aircraft configurations

Author
Craidon, C. B.
Published
Nov 1, 1983.
Physical Description
1 electronic document
Online Version

Availability

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
A computer program was developed to extend the geometry input capabilities of previous versions of a supersonic zero lift wave drag computer program. The arbitrary geometry input description is flexible enough to describe almost any complex aircraft concept, so that highly accurate wave drag analysis can now be performed because complex geometries can be represented accurately and do not have to be modified to meet the requirements of a restricted input format.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19840003706.
Accession ID: 84N11774.
NAS 1.15:85670.
L-15603.
NASA-TM-85670.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15711097