Search

Advanced search

Normal view MARC view ISBD view

The effects of leading-edge serrations on Reducing flow unsteadiness about airfoils : an experimental and analytical invertigation [NASA CR-2344]

By: Schwind, R. G.

Contributor(s): Allen, H. J.

Material type: materialTypeLabel

materialTypeLabel

BookSeries: National Aeronautics and Space Administration (NASA). Publisher: Nasa Washington, D. C. 1973Description: 97p.Subject(s): Aerofoils

Contents:

NASA technical report

average rating: 0.0 (0 votes)

Holdings ( 1 )
Title notes
Comments ( 0 )

Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)	NASA CR-2344 (Browse shelf)	Not for loan		TR101615(e)

Total holds: 0

Browsing PK Kelkar Library, IIT Kanpur Shelves , Collection code: COMPACT STORAGE (BASEMENT) Close shelf browser

Previous								Next
Previous	NASA CR-2340 Research on the sonic boom problem [ Part 2]	NASA CR-2341 Quantitative understanding of explosive stimulus transfer [NASA CR-2341]	NASA CR-2343 The radiometer transfer function for the AAFE composite two-frequency radiometer scatterometer. M.S. Thesis - Pennsylvania Univ. [NASA CR-2343]	NASA CR-2344 The effects of leading-edge serrations on Reducing flow unsteadiness about airfoils	NASA CR-2345 The development of a pseudo-nyquist analysis technique for hybrid sampled-data control systems [NASA CR-2345]	NASA CR-2346 A methodology for boost- glide transport technology planning [NASA CR-2346]	NASA CR-2348 A test technique for measuring lightning	Next

NASA technical report

There are no comments for this item.

Log in to your account to post a comment.

Powered by Koha