Aircraft Engineering and Aerospace Technology: Volume 28 Issue 7
Strapline:
An International JournalTable of contents
Fatigue Problems
IN this issue we publish a translation (by MR TIBOR HAAS, whom readers will remember as the author of the paper ‘Fatigue Tests and Aircraft Life Evaluation’ in our October 1955…
The Design of Wing Sections: A Survey of Existing Knowledge on Aerofoil Design for Different Conditions
T. NonweilerIS there anything magic about the shape of a wing section? Asked to sketch the profile of a wing on the back of an envelope, one would have no difficulty in representing a shape…
The Problem of Fatigue Strength in Aircraft Structures: A Survey with Recommendations for Design Rules based on Recent Research
Ing. E. GassnerIN aircraft construction, until about fifteen years ago, the customary static method of stressing generally also provided for an adequate fatigue strength. This does not now apply…
Turbine Disks for Jet Propulsion Units: An Account of Work of the Disk Panel of the Ministry of Supply, Gas Turbine Collaboration Committee, during the years 1941–1949
A.E. JohnsonTHREE methods of elastic stress computation are described in the following section.
Automatic Machine Tool Control Systems: A Brief Account of the Potentialities of Two British Electronic Systems
MUCH thought about the automatic control of machine tools has been confused by an imperfect understanding of what can be done, and of what the advantages of the various systems…
The Library Shelf
E.G.B., A.R.F.The subject of aeroelasticity is not well provided with text books and this makes the present book all the more valuable. One difficulty in writing such a text book is that…
Trade Announcements
The British Tabulating Machine Company Limited announces that it has recently concluded arrangements with Laboratory for Electronics Inc. of Boston, U.S.A., for the joint…
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…
Month in the Patent Office
In an arrangement for deflecting a propulsive jet forwardly for braking purposes the jet reversal is effected by moving a series of curved blades at the rear end of the jet pipe…
U.S. Patent Specifications
In an aeroplane, in combination with an aerofoil, a control surface located at the trailing edge of said aerofoil, means mounting said control surface for movement from a normal…
ISSN:
0002-2667Online date, start – end:
1929Copyright Holder:
Emerald Publishing LimitedOpen Access:
hybridEditor:
- Prof Phil Webb