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A theoretical investigation into the lateral stability of an aeroplane controlled by an automatic pilot, with particular reference to the effect of flight path angle / by T.W. Prescott.

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Bibliographic Details
Main Author:	Prescott, T. W.
Corporate Author:	Aeronautical Research Council (Great Britain)
Format:	Book
Language:	English
Published:	London : H.M.S.O, 1952.
Series:	Reports and memoranda (Aeronautical Research Council (Great Britain)) ; no. 2640.
Subjects:	Stability of airplanes, Lateral > Mathematical models. Automatic pilot (Airplanes)

Norlin Library - Basement - Government Information - Foreign

Holdings details from Norlin Library - Basement - Government Information - Foreign
Call Number:	301-Ae8 4:
301-Ae8 4: (2626-2649)	Available Place a Hold Contents The following works are all found in the book indicated by the call number above. A theoretical investigation into the lateral stability of an aeroplane controlled by... The use of tensor notation to develop characteristic equations of supersonic flow / b... The derivation of airworthiness performance climb standards / by F.G.R. Cook and A.K.... An experimental investigation on the flutter characteristics of a model flying wing /... Comparative flutter tests on two, three, four and five-blade propellers / by H.G. Ewi... Wind-tunnel tests on the 30 per cent symmetrical Griffith aerofoil with distributed s... The buckling in compression of panels with square top-hat section stringers / by W.S.... Notes on the design of converging channels / by S. Goldstein. The induced velocity field of a rotor / by K.W. Mangler and H.B. Squire. Heat transference and pressure loss for air flowing in passages of small dimensions /... Regenerator heat exchangers for gas-turbines / by J.E. Johnson. Performance calculations for a double-compound turbo-jet engine of 12:1 design compre... Reports and memoranda / Aeronautical Research Council. Towing-tank tests on a large six-engine flying boat seaplane, to specification 10/46... A comparison between plain and stringer-reinforced sheet from the shear lag standpoin... The dynamic landing loads of flying boats with special reference to measurements made... Wind-tunnel tests on a thick suction aerofoil with a single slot / M.B. Glauert, [and... Model tests in the 24-ft wind tunnel to determine the optimum angle for release of a... Four- and eight-channel Desynn graphical recorders / by F.R.J. Spearman. Speeds and normal accelerations of Boeing "Clipper" aircraft on North and South Atlan... A criterion for the prevention of spring-tab flutter / by A. R. Collar and G. D. Shar... 24-ft tunnel tests on a high-lift model : downwash and velocity measurements at the t... Boundary-layer flow along a flat plate with uniform suction. Model tests on an air interchange system for removing engine exhausts products from a...