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The application of the exact method of aerofoil design / by M.B. Glauert.

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Bibliographic Details
Corporate Author:	Aeronautical Research Council (Great Britain)
Other Authors:	Glauert, M. B.
Format:	Book
Language:	English
Published:	London : H.M.S.O, 1955.
Series:	Reports and memoranda (Aeronautical Research Council (Great Britain)) ; no. 2683.
Subjects:	Aerofoils > Design and construction.

Norlin Library - Government Information - US

Holdings details from Norlin Library - Government Information - US
Call Number:	301-Ae8 4:2676-2700
301-Ae8 4:2676-2700	Available Place a Hold Contents The following works are all found in the book indicated by the call number above. Measurements of mid-chord pitching moment derivatives at high speeds / by J.B. Bratt... High-speed tunnel tests of a 5 per cent. chord dive-recovery flap on a NACA 0015 aero... An electric tank for the determination of theoretical velocity distributions / by T.J... General performance calculations for gas turbine engines / D.H. Mallinson. Sandwich construction and core materials. Part V / by W. J. Pullen. Note on the Southwell method for estimating critical loads, / by H.L. Cox. Sandwich construction and core materials. Part VI (in three sections) / by W. J. Pull... Some investigations on thin nose-suction aerofoils. Parts 1 and 2 / by J. Williams. The application of the exact method of aerofoil design / by M.B. Glauert. Some high-speed tests on turbine cascades / by E.A. Bridle. Some tests on compressor cascades of related aerofoils having different positions of... Proposal for an Elevator Manœuvrability Criterion. Experiments giving hinge moment and lift on a NACA 0015 aerofoil fitted with a 40 per... A theoretical examination of the effect of deadrise on wetted area and associated mas... The pressure distribution, at supersonic speeds and zero lift, on some swept-back win... The correlation of aeroplane loading and accident statistics / by A.G. Pugsley. Notes on the tail-first aeroplane / by S.B. Gates. Wind-tunnel tests on a 12-ft diameter helicopter rotor / by H. B. Squire; R. A. Fail... Measurements of maximum lift on 26 aerofoil sections at high mach number. Part I, Tes... Photographs of shock wave movement / by W.F. Hilton and R.G. Fowler. A revised index of mathematical tables for compressible flow / by R.C. Tomlinson. A comparison of two methods of calculating wing loading with allowance for compressib... Service failures in aircraft structures associated with fatigue, repeated or dynamic... The Royal Aircraft Establishment 4 ft x 3 ft experimental low turbulence wind tunnel....