Aircraft Engineering and Aerospace Technology: Volume 25 Issue 3
Strapline:
An International JournalTable of contents
Planning for Output
WE conclude in this issue the publication of the papers read at the Southampton conference on the problem of aircraft production; the first two of which appeared in AIRCRAFT…
The Peeling Test on Redux‐bonded Joints: A Theoretical Analysis of the Test Devised by Aero Research Limited
G.J. SpiesA theoretical analysis is given of the peeling test for Redux‐bonded joints, as devised by Aero Research Ltd. and generally accepted as a standard quality control test for…
The Library Shelf
A.R.C.The present reviewer was privileged to see the manuscript of this book some three or four years before its publication. It is a pleasure, therefore, to record that in its final…
The Length of Aerofoil Curved Surfaces: A Method for the Rapid Calculation of the Length of the Periphery of an Aerofoil Surface
V.M. FalknerIN applied aeronautics it is frequently necessary to calculate the distance along the curved surface of an aerofoil, not only for constructional purposes, but also in order to…
Problems of Aircraft Production
The paper which I have prepared on the subject of ‘Prototype to Production’ will deal with the forward planning and control necessary to guide a new aircraft through its various…
Auxiliary Equipment
Motor Generator Corporation, Hobart Brothers Affiliate, Troy, Ohio, U.S.A., produces motor generator frequency changers in 3, 5 and 10 kW. sizes for aircraft use to operate test…
Research Reports and Memoranda
Under this heading are published regularly abstracts of all Reports and Memoranda of the Aeronautical Research Council, Reports and Technical Memoranda of the United States…
Trade Announcements
The British Aluminium Co. Ltd. announce that they have vacated their Branch Office and Warehouse at 66 Kirkstall Road, Leeds, 3, and have transferred their Branch Office to…
Month in the Patent Office
An aircraft undercarriage comprises a four‐wheeled bogie, of which two of the wheels, 16, 17, are independently rotatable and are mounted on a common transverse axle 15 at the…
U.S. Patent Specifications
A propulsion device for assisting an aircraft in take‐off, comprising a substantially cylindrical casing open at one end, a back end plate acting to close said open end, a nozzle…
ISSN:
0002-2667Online date, start – end:
1929Copyright Holder:
Emerald Publishing LimitedOpen Access:
hybridEditor:
- Prof Phil Webb