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A preliminary study of effects of Reynolds number and boundary layer transition location on shock-induced separation [NASA TN D-5003]

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BookSeries: National Aeronautics and Space Administration (NASA). Publisher: Washington, D.C. NASA 1969Description: 25p.Subject(s): Reynolds numberSummary: NASA technical note D-5003

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		Not for loan		TR10416 [D-5003}

Total holds: 0

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Previous	NASA Technical Note [NASA TN D-1943]: A method for predicting the static strength of a stiffened sheet containing a sharp central notch	Analytical study of flow reduction due to oxidation of wire from porous sheet for transpiration cooled turbine blades [NASA TN D-5001]	Rolling element bearing life from 400 degree to 600 degree [NASA TN D-5002]	A preliminary study of effects of Reynolds number and boundary layer transition location on shock-induced separation [NASA TN D-5003]	Roughness drag due to two-dimensional fabrication type surface roughness on an ogive cylinder from force tests at transonic speeds [NASA TN D-5004]	NASA TN [D-4166]	Structural weight analysis of hypersonic aircraft [NASA TN D-6692]	Next

NASA technical note D-5003

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