Laminar boundary layer on a spinning circular cone in supersonic flow at a small angle of attack,

Laminar boundary layer on a spinning circular cone in supersonic flow at a small angle of attack,

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Bibliographic Details
Corporate author / creator:	Cornell University. Graduate School of Aeronautical Engineering.
Imprint:	Ithaca, N.Y., 1956-
Description:	v.
Language:	English
Subject:	Aerodynamics, Supersonic. Laminar boundary layer.
Format:	Print Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/4134946

Hidden Bibliographic Details
Other authors / contributors:	Fiebig, Martin. United States. Air Force. Office of Scientific Research. Mechanics Division
Notes:	Prepared for contract no. AF 18 (600)-1523. AFOSR TN56-532, TN57-68; ASTIA no. AD110351, AD-120-410.

Crerar, Lower Level, Dewey Collection

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Holdings details from Crerar, Lower Level, Dewey Collection
Call Number:	TE3a 628 c.1
Issues:	1956:Jun,1957:Feb
c.1 : 1956 Jun	Available Loan period: standard loan Scan and Deliver Request for Pickup Need help? - Ask a Librarian
c.1 : 1957 Feb	Available Loan period: standard loan Scan and Deliver Request for Pickup Need help? - Ask a Librarian