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The geared elevator tab and tail-unit stiffness requirements / by Ll. T. Niblet.

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Bibliographic Details
Main Author:	Niblett, Ll. T.
Corporate Authors:	Aeronautical Research Council (Great Britain), Royal Aircraft Establishment (Great Britain)
Format:	Book
Language:	English
Published:	London : H.M.S.O, 1955.
Series:	Reports and memoranda (Aeronautical Research Council (Great Britain)) ; no. 2848.
Subjects:	Elevators (Airplanes) > Mathematical models. Airplanes > Tail surfaces > Mathematical models.

Norlin Library - Basement - Government Information - Foreign

Holdings details from Norlin Library - Basement - Government Information - Foreign
Call Number:	301-Ae8 4:
301-Ae8 4: (2826-2849)	Available Place a Hold Contents The following works are all found in the book indicated by the call number above. Simple evaluation of the theoretical lift slope and aerodynamic centre of symmetrical... Low-speed wind-tunnel tests on a model of a jet tailless aircraft / by J. Trouncer an... The manoeuvrability of aircraft in circling flight / by H.L. Price. Alternating pressures and blade stresses in an axial-flow compressor / by J.R. Forsha... The effect of uniformly spaced flexible ribs on the stresses due to self-equilibratin... A theoretical approach to the design of hydrofoils / by C.H.E. Warren. The turbulent boundary layer in compressible flow / by W.F. Cope. Pressure plotting and balance measurements in the high speed wind tunnel on a half-mo... Aerodynamic coefficients for an oscillating delta wing / by Doris E. Lehrian. The theoretical wave drag of some bodies of revolution / by L.E. Fraenkel. Symmetric flutter characteristics of a hypothetical delta wing / D.L. Woodcock. Report on the flow phenomena at supersonic speed in the neighbourhood of the entry of... The influence of rolling moments on spin recovery as observed in model-spinning tests... Detailed observations made at high incidences and at high-subsonic mach numbers on Go... The stress distribution in a swept-back box-beam with perpendicular ribs / by P.B. Ho... The geared elevator tab and tail-unit stiffness requirements / by Ll. T. Niblet. Aerofoil design in two-dimensional subsonic compressible flow / L.C. Woods. Reports and memoranda / Aeronautical Research Council. An experimental investigation of the boundary layer on a porous circular cylinder / b... Towing-tank tests on a large six-engine flying boat seaplane, to specification 10/46... An unconventional type of fatigue-testing machine / by F. Aughtie and H.L. Cox. Kinetic temperature of wet surfaces : a method of calculating the amount of alcohol r... Flutter problems of high-speed aircraft / by E.G. Broadbent. Flight trials of a rocket-propelled transonic research model : the R.A.E.-Vickers roc...