Cover Image

Reports and memoranda / Aeronautical Research Committee.

Show other versions (1)

Saved in:

Bibliographic Details
Online Access:	Connect to online resource Request a PDF (UCB only)
New Title:	Reports and memoranda (Aeronautical Research Council (Great Britain))
Previous Title:	Reports and memoranda (Great Britain. Advisory Committee for Aeronautics)
Corporate Author:	Great Britain. Aeronautical Research Committee
Other Authors:	Cope, W. F., Goldștein, Ș., Sargent, R. F., Preston, J. H., Simmons, L. F. G., Fage, A. (Arthur), Cowley, W. L. (William Lewis), 1890-
Other title:	Reports and memoranda (Great Britain. Aeronautical Research Committee) Reports and memoranda (Great Britain. Advisory Committee for Aeronautics) Test on a large aerofoil of R.A.E. 15 Section Contribution of the separate planes to the forces on a biplane (R.A.F.15 Section) Biplane investigation with R.A.F.15 Section Equations of hydrodynamics in a very general form Linear perturbation theory of compressible flow, with applications to wind-tunnel interference Effect on aerofoil drag of boundary-layer suction behind a shock wave Note on errors arising in measurements of turbulence Interference on a wing spanning a closed tunnel arising from the boundary layers on the side walls, with special reference to the design of two-dimensional tunnels
Format:	Serial
Language:	English
Published:	London : H.M.S.O., 1921-[1944?]
Subjects:	Aeronautics. Aeronautics > Research > Great Britain. Aerodynamics > Mathematical models.

Internet

Connect to online resource
Request a PDF (UCB only)

Norlin Library - Basement - Government Information - Foreign

Holdings details from Norlin Library - Basement - Government Information - Foreign
Call Number:	301-Ae8 1: 301-Ae8 4:
Volume Holdings:	95,100-140,145 (1913-14)
Notes:	497,557,575,589,598,609,708,720,731,767,774,824,837,857,872,888-889,901,917,996,1311,1467,1581,1591,1593-1594,1596,1651-1653,1655-1656,1667,1727,1832,1839,1842,1844,1849,1854,1861,1865-1867,1872-1875,1877-1883,1900,1902-1992
301-Ae8 1: (589 1919)	Available Place a Hold
301-Ae8 1: (774 1922)	Available Place a Hold
301-Ae8 1: (857 1923)	Available Place a Hold
301-Ae8 1: (872 1923)	Available Place a Hold
301-Ae8 1: (888 1924)	Available Place a Hold
301-Ae8 1: (1950 (List 1851-1950 1939-45))	Available Place a Hold
301-Ae8 4: (1902-1925)	Available Place a Hold Contents of [301-Ae8 4:] The following works are all found in the book indicated by the call number above. The stabilization of struts by lateral support / by H.L. Cox. Wind tunnel interference effect on the values of experimentally determined derivative... The response of an aeroplane to the application of ailerons and rudders. Part I, Resp... Reports and memoranda / Aeronautical Research Committee. A philosophy of aeroplane strength factors / by A.G. Pugsley. Natural frequencies of vibration for a wing carrying engines / by G.C.J. Dalton ... F... Steady two-dimensional flow past a solid cylinder in a non-uniform stream, and, Two-d... Wood stringer sandwich construction. A method for the rapid evaluation of Glauert's expressions for the angle of zero lift... The renewal of aircraft / by D.J. Bishop. Rational stressing cases for symmetric flight / by P.B. Walker. A simple method of constructing stability diagrams / by W.S. Brown. Measurements of pitching moment derivatives for an aerofoil oscillating about the hal... Note on errors arising in measurements of turbulence / by L.F.G. Simmons. A theoretical analysis of the impact of an elastic body on water / by S.V. Fagg. Calculations of derivatives for rectangular wings of finite span by Cicala's method /... The representation of aircraft wings, tails, and fuselages by semi-rigid structure in... On the stressing of polygonal tubes with particular reference to the torsion of taper... The calculation of aerodynamic loading on surfaces of any shape / by V.M. Falkner. Note on the calculation of vibration frequencies for an aero-engine installation / by...

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	301-Ae8 4:
Volume Holdings:	1560
301-Ae8 4: (1560)	Restricted Place a Hold

Online

Holdings details from Online
Call Number: