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A New Blade Element Method for Calculating the Performance of Hi

(Tech/propulsion/fan:NASA-CR-3063) Borst, Henry V.: A New Blade Element Method for Calculating the Performance of High and Intermediate Solidity Axial Flow Fans. This is an attempt to expand the "isolated airfoil" method of fan design into a method covering the entire range of fan solidities and disc loadings. We haven't tested this scheme yet. Useful for the bibliography alone!, NASA, Contractor Reports. 1978. 48 pages. Electronic master; price based on download or delivery on CD; see Options below for paper copies, binding. Price: $4.90

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This product was added to our catalog on Saturday 23 October, 2010.
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