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HSCT mission analysis of waverider designsIn the second quarter the development of the two waverider design tools was continued, and the groundwork necessary for the incorporation of waverider technology into the realm of the High Speed Civil Transports (HSCT's) was laid out. Advances in each of these areas is summarized. Work on the WIPAR code included the addition of an upper surface geometry generator and characteristic flow solver and the inclusion of viscous analysis in the performance computations. Details of these changes are given. In the course of the second project quarter, much of the analysis performed during the first quarter was incorporated into a working computer code. To date, utilities were developed for the definition of arbitrary 3-D shock surfaces, the computation of post-shock flow conditions, and the marching of the solution in a roughly cross-stream direction away from the shock surface. These utilities are briefly described. During the second quarter groundwork for the analysis of complete configurations was initiated. This involved the development of computational utilities for the integration of powerplants with the waverider forebodies, and the acquisition of a number of configuration analysis software packages. Work in these areas is discussed.
Document ID
19930012457
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 6, 2013
Publication Date
November 15, 1992
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
REPT-153-6442
NASA-CR-192193
NAS 1.26:192193
Report Number: REPT-153-6442
Report Number: NASA-CR-192193
Report Number: NAS 1.26:192193
Accession Number
93N21646
Funding Number(s)
CONTRACT_GRANT: NAG1-1295
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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