Aircraft Engineering and Aerospace Technology: Volume 30 Issue 10

Strapline:

An International Journal
Subjects:

Table of contents

After the Show

OUR first issue after Farnborough appears, as always, after the events of the show week have ceased to be fresh in the memory. A few details which caught our eye are presented…

The Shear Modulus of Foil Honeycomb Cores: A Theoretical and Experimental Investigation on Cores Used in Sandwich Construction

S. Kelsey, R.A. Gellatly, B.W. Clark

Simple expressions for upper and lower limits to the shear modulus of honeycomb sandwich cores are obtained by application of the Unit Displacement and Unit Load methods in…

1645

Farnborough 1958

Photographs of a Selection of Exhibits at the 1958 S.B.A.C. Display

The Solution of ‘Ill‐Conditioned’ Linear Simultaneous Equations: Methods for Reducing the Influence of Experimental Errors

J.W. Head, G.M. Oulton

When linear simultaneous equations are ‘ill‐conditioned’, small variations in the (usually measured) quantities on the right‐hand sides of the equations are associated with large…

Simple Shielded Total‐Pressure Probes: Details of Small Probes with Results of Tests on their Performance

F.A.L. Winternitz

Design features and characteristics of conventional, modified and shielded total‐pressure probes are briefly discussed, and compared with new shielded instruments of simple…

The Library Shelf

S.L.K., E.G.B.

This book is an important study of the clastic behaviour of thin wings subjected to non‐linear temperature gradients and particularly valuable are the numerous experimental…

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

A piston‐and‐cylinder friction type vibration damper 16 is disposed between each pair of adjacent rotor blades 10 of a helicopter rotor. There is no damper provided at the drag…

U.S. Patent Specifications

In a rotary wing aircraft having a fuselage and two load‐carrying rotors turning in opposite directions and having rotor blades of aerofoil cross section, means for controlling…

Cover of Aircraft Engineering and Aerospace Technology

ISSN:

0002-2667

Online date, start – end:

1929

Copyright Holder:

Emerald Publishing Limited

Open Access:

hybrid

Editor:

  • Prof Phil Webb