Turboduct prop advantageous for 0 to 0.06 Mach aircraft.

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Bibliographic Details
Title: Turboduct prop advantageous for 0 to 0.06 Mach aircraft.
Authors: Cahn, M. S.
Source: Sae Journal; March 1963, Vol. 71, p88-90, 3p
Database: Applied Science & Technology Source
Description
ISSN:0036066X