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Investigation at low speed of a six-percent thick symmetrical circular-arc airfoil with leading edge retraction in combination with nose slot /

Thesis (Aeronautical Engineer). / Includes bibliographical references.

Identiferoai:union.ndltd.org:OCLC/oai:xtcat.oclc.org:OCLCNo/437058796
Date January 1955
CreatorsBirdwell, Carl. Stewart, Homer Joseph, Roshko, A.
PublisherPasadena, Calif. : California Institute of Technology,
Source SetsOCLC
LanguageEnglish
Detected LanguageEnglish
TypeElectronic dissertations.
Source<a href="http://resolver.caltech.edu/CaltechETD:etd-12022003-154259" TARGET="_blank">Investigation at Low Speed of a Six-percent Thick Symmetrical Circular-arc Airfoil with Leading Edge Retraction in Combination with Nose Slot [electronic thesis]</a>

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