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The effect of sting interference at low speeds on the drag coefficient of an ellipsoidal body using a magnetic suspension and balance systemA Boltz body of revolution (fineness ratio 7.5:1) was tested in the Southampton University Magnetic Suspension and Balance System. The effects of sting interference on the drag coefficient of the model at zero angle of attack were noted as well as the effects on drag coefficient values at boundary layer trips. The drag coefficient values were compared with other sources and seemed to show agreement. The pressure distribution over the rear of the model with no sting interference was investigated including the use of boundary layer trips.
Document ID
19880010890
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Newcomb, A. W.
(Vigyan Research Associates, Inc. Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1988
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-181611
NAS 1.26:181611
Report Number: NASA-CR-181611
Report Number: NAS 1.26:181611
Accession Number
88N20274
Funding Number(s)
CONTRACT_GRANT: NAS1-17919
PROJECT: RTOP 505-61-01-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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