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The pressure in a two-dimensional static hole at low Reynolds numbers / by A. Thom and C.J. Apelt.

A description is given of an arithmetical method for obtaining solutions for steady incompressible viscous flow at low Reynolds numbers in the form of expansions in powers of the Reynolds numbers.

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Bibliographic Details
Main Author:	Thom, A. (Alexander), 1894-1985
Corporate Author:	Aeronautical Research Council (Great Britain)
Other Authors:	Apelt, C. J. (Colin James)
Format:	Book
Language:	English
Published:	London : H.M.S.O, 1958.
Series:	Reports and memoranda (Aeronautical Research Council (Great Britain)) ; no. 3090.
Subjects:	Viscous flow > Mathematical models. Aerodynamics > Mathematical models. Reynolds number.

Norlin Library - Basement - Government Information - Foreign

Holdings details from Norlin Library - Basement - Government Information - Foreign
Call Number:	301-Ae8 4:
301-Ae8 4: (3076-3100 (lacks 3088))	Available Place a Hold Contents The following works are all found in the book indicated by the call number above. The representation of engine airflow in wind-tunnel model testing / by J. Seddon and... Observations of the flow past a two-dimensional 4 per cent thick biconvex aerofoil at... The wave drag of non-lifting combinations of thin wings and 'non-slender' bodies / by... The development of slotted working-section liners for transonic operation of the R.A.... A case of longitudinal stick-free dynamic instability of an aircraft fitted with powe... Experiments with a two-dimensional aerofoil designed to be free from turbulent bounda... Low-speed-tunnel model tests on the flow structure behind a delta-wing aircraft and a... The full-scale air drag of some flying-boat seaplanes / by A.G. Smith. Observations of the flow patterns of a two-dimensional 4 per cent thick biconvex aero... Experiments on the use of suction through perforated strips for maintaining laminar f... Thermodynamic data for the calculation of gas turbine performance / by D. Fielding an... All-moving wing-tip controls at subsonic, sonic and super-sonic speeds : A discussion... An analysis of steady straight flight with inclined thrust / by S.B. Gates and A.W. T... An investigation of the hydrodynamic stability and spray characteristics of high leng... The development of a variable Mach-number effuser / by J.B. McGarry. Supersonic wind-tunnel flutter tests of two rectangular wings / by P.R. Guyett. Some factors influencing the speed of response of hydraulic position servomechanisms... The pressure in a two-dimensional static hole at low Reynolds numbers / by A. Thom an... Methods for determining the wave drag of non-lifting wing-body combinations / by L. M... Wind-tunnel tests on the effect of body freedoms on the flutter of a model wing carry... The R.A.E. Hollerith punched-card installation (1945-1952) / by R.A. Fairthorne, Miss... Pressure-plotting measurements on an 8 per cent thick aerofoil with trailing-edge fla... An experimental investigation of leading-edge flow separation from a 4 percent thick... The shape of the centre part of a swept-back wing with a required load distribution /...