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Method to predict external store carriage characteristics at transonic speedsDevelopment of a computational method for prediction of external store carriage characteristics at transonic speeds is described. The geometric flexibility required for treatment of pylon-mounted stores is achieved by computing finite difference solutions on a five-level embedded grid arrangement. A completely automated grid generation procedure facilitates applications. Store modeling capability consists of bodies of revolution with multiple fore and aft fins. A body-conforming grid improves the accuracy of the computed store body flow field. A nonlinear relaxation scheme developed specifically for modified transonic small disturbance flow equations enhances the method's numerical stability and accuracy. As a result, treatment of lower aspect ratio, more highly swept and tapered wings is possible. A limited supersonic freestream capability is also provided. Pressure, load distribution, and force/moment correlations show good agreement with experimental data for several test cases. A detailed computer program description for the Transonic Store Carriage Loads Prediction (TSCLP) Code is included.
Document ID
19880018650
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rosen, Bruce S.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1988
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:4170
NASA-CR-4170
Report Number: NAS 1.26:4170
Report Number: NASA-CR-4170
Accession Number
88N28034
Funding Number(s)
CONTRACT_GRANT: NAS1-18105
PROJECT: RTOP 505-60-21-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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