Measurement of unsteady blade surface pressure on a single rotation large scale advanced prop-fan with angular and wake inflow at mach numbers from 0.02 to 0.70 [microform] / P. Bushnell, M. Gruber, and D. Parzych.

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Bibliographic Details
Main Author:	Bushnell, Peter
Corporate Author:	United States. National Aeronautics and Space Administration
Other Authors:	Gruber, M., Parzych, D.
Format:	Government Document Microfilm Book
Language:	English
Published:	[Washington, DC] : National Aeronautics and Space Administration, [1988]
Series:	NASA contractor report ; NASA CR-182123.
Subjects:	Propellers.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.26:182123
NAS 1.26:182123	Restricted Place a Hold