High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions [microform] / Julio Chu and Pierce L. Lawing.

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Bibliographic Details
Main Author:	Chu, Julio
Corporate Author:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Other Authors:	Lawing, Pierce L.
Other title:	High Reynolds number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions. High-Reynolds-number test of a five-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wind tunnel distributions.
Format:	Government Document Microfilm Book
Language:	English
Published:	[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1990.
Series:	NASA technical memorandum ; 4227.
Subjects:	Airplanes > Wings. Transonic wind tunnels.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.15:4227
NAS 1.15:4227	Restricted Place a Hold