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Boundary layer and wake investigation in supersonic flow / by J. Lukasiewicz and J.K. Royle.

Describes the results of traverses of the boundary layer and wake encountered in a small supersonic tunnel at a Mach number of 2.5.

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Bibliographic Details
Online Access:	Online Access
Main Author:	Lukasiewicz, J.
Corporate Author:	Aeronautical Research Council (Great Britain)
Other Authors:	Royle, J. K.
Format:	Book
Language:	English
Published:	London : H.M.S.O, 1952.
Series:	Reports and memoranda (Aeronautical Research Council (Great Britain)) ; no. 2613. A.R.C. technical report.
Subjects:	Aerodynamics, Supersonic. Supersonic wind tunnels. Wall pressure (Aerodynamics) Wakes (Aerodynamics)

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Holdings details from Online
Call Number:	301-Ae8 4:2613
301-Ae8 4:2613	Available

Norlin Library - Basement - Government Information - Foreign

Holdings details from Norlin Library - Basement - Government Information - Foreign
Call Number:	301-Ae8 4:
301-Ae8 4: (2601-2625 1951-52)	Available Place a Hold Contents The following works are all found in the book indicated by the call number above. Flutter of control surface tabs / by G.A. Naylor. 24-ft wind tunnel tests on a propeller with NACA 16 series sections : test results an... The flow in an axially-symmetric supersonic jet from a nearly-sonic orifice into a va... Estimation of wing flutter speeds from the curves of R. & M. 1869 / by Mary E.K. Grah... Boundary layer and wake investigation in supersonic flow / by J. Lukasiewicz and J.K.... Some preliminary results from V-g recorders installed in military and civil aircraft... The production of lift independently of incidence : the Thwaites Flap / by B. Thwaite... Tests on a whirlwind aircraft in the Royal Aircraft Establishment 24-ft. wind tunnel... A résumé of aerodynamic data on air brakes / by H. Davies and F.N. Kirk. Contra-flow turbo-compressor tests / by A.D. Baxter and C.W.R. Smith. Reports and memoranda / Aeronautical Research Council. On the design of aerofoils for which the lift is independent of the incidence. A method of estimating the direct stress concentration round holes in reinforced shee... The numerical method of characteristics for hyperbolic problems in three independent... A review of some stalling research / by A.D. Young: with an appendix on wing section... Theoretical velocity distribution in a high-speed tunnel contraction / by M. Jones &...