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The icing of compressor blades, and their protection by surface heating / by G.L. Shires and G.E. Munns.

Describes an investigation into the feasibility of protecting compressor blades against ice accretion by surface heating.

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Bibliographic Details
Main Author:	Shires, G. L.
Corporate Author:	Aeronautical Research Council (Great Britain)
Other Authors:	Munns, G. E.
Format:	Book
Language:	English
Published:	London : H.M.S.O, 1958.
Series:	Reports and memoranda (Aeronautical Research Council (Great Britain)) ; no. 3041.
Subjects:	Airplanes > Ice prevention. Compressors > Blades > Heating. Aircraft icing. Ice prevention. Deicing.

Norlin Library - Basement - Government Information - Foreign

Holdings details from Norlin Library - Basement - Government Information - Foreign
Call Number:	301-Ae8 4:
301-Ae8 4: (3026-3049 1953-57)	Available Place a Hold Contents The following works are all found in the book indicated by the call number above. Calculated velocity distributions and force derivatives for a series of high-speed ae... Experiments at M=1.41 on elliptic cones with supersonic leading edges / by E.W.E. Rog... Experimental and theoretical investigations of the flow of air through two single-sta... The influence of plain bearings on shaft whirling / by E. Downham. A numerical method for calculating the starting and perturbation of a two-dimensional... The calculation of the pressure distribution on the surface of thick cambered wings a... The theoretical determination of normal modes and frequencies of vibration / by I.T.... On some aspects of the use of shock tubes in aerodynamic research. Theory of aerofoils on which occur bubbles of stationary air / by L.C. Woods. A method for calculating the pressure distribution over jet-flapped wings / by D. Küc... A general method (depending on the aid of a digital computer) for deriving the struct... Some actuator-disc theories for the flow of air through an axial turbo-machine / by J... An investigation of the velocity distribution around the nose of the aerofoil with a... Measurements of two-dimensional derivatives on a wing-aileron-tab system with a 1541... Pressure probes selected for three-dimensional flow measurement / by D.W. Bryer, D.E.... The icing of compressor blades, and their protection by surface heating / by G.L. Shi... A survey and correlation of data on heat transfer by forced convection at supersonic... The matrix force method of structural analysis and some new applications / by Profess... The estimation of shock pressure recovery and external drag of conical centre-body in... The effects of taper on the supervelocities on three-dimensional wings at zero incide... Tests in the Royal Aircraft Establishment 10-ft X 7-ft high-speed tunnel on ... / by... Experiments on pitot-tubes in shear flow / by F.A. MacMillan ; communicated by the Di... The harmonically oscillating wing with finite vortex trail / by P.F. Jordan. Current tests on laminar-boundary-layer control by suction through perforations / by...