Aircraft Engineering and Aerospace Technology: Volume 26 Issue 12

Strapline:

An International Journal
Subjects:

Table of contents

To Altitude and Back

THE causes of the crashes of the two Comets are not yet subjects for comment since, being at present under investigation by the British Court of Inquiry, they must be treated as…

Wings Under Repeated Thermal Stress: Permanent Elasticity, Shakedown, Alternate Plasticity and Incremental Collapse in Wings Subjected to a Number of Thermal Cycles

E.W. Parkes

When an aircraft changes its speed or altitude, large thermal strains may be set up in the wing structure; sometimes these are of sufficient magnitude for the accompanying…

The Shock‐Wave Cubic: Presentation of an Equation which Permits the Solution of Shock‐Wave Problems without Tables

V.D. Naylor

The inverse problem of finding the shock‐wave angle when a supersonic stream passes round a bend of (180°—i°) involves a double interpolation from tables prepared for the direct…

The Library Shelf

The advent of jet and rocket propulsion in our present age has brought the problems of combustion right into the foreground. While much is known, still more theoretical and…

Sponsored Research on Light Alloys: A Note on Current Work of the Fulmer Research Institute

A.G. Thomson

PROMINENT members of the aircraft industry were among more than 300 people present at the Fulmer Research Institute, on November 2, when a new engineering laboratory was opened by…

S.A.E. National Los Angeles Aeronautic Meeting: Summaries of Papers Presented at the Meeting Held in Los Angeles, California, on October 5–9, 1954

Discusses some of the stability, control and operational problems arising in the design of supersonic aircraft. The changes in the flow patterns about an aerofoil as a function of…

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

An aircraft structural member such as a wing or fuselage is provided with a series of suction ducts formed in transversely disposed structural elements and embodying porous…

U.S. Patent Specifications

Propulsive thrust generating apparatus having forward propulsive thrust reacting surfaces comprising: a duct; means for introducing into said duct a plurality of fluids which…

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