The computation of aerodynamic loads on helicopter blades in forward flight, using the method of the accelerationpotential.

Description

Thesis - Technische hogeschool Delft. / Bibliography: p. 108.

Links & Downloads

1. http://dds.crl.edu/CRLdelivery.asp?tid=12646

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Additional Fields

Identifer	oai:union.ndltd.org:OCLC/oai:xtcat.oclc.org:OCLCNo/13572738
Date	January 1900
Creators	Holten, Th. van.
Publisher	Rotterdam,
Source Sets	OCLC
Language	English
Detected Language	English
Source	Online version