Aircraft Engineering and Aerospace Technology: Volume 26 Issue 3

Strapline:

An International Journal
Subjects:

Table of contents

A Milestone

THE austere columns of AIRCRAFT ENGINEERING do not lend themselves to special numbers in celebration of milestones in its own domestic history but we feel that it should be put on…

The Elementary Theory of Aero‐Elasticity: A Series of Articles Written from the Standpoint of a Structural Engineer for Students and junior Members of Aircraft Design Teams

E.G. MA Broadbent, A.F.R.Ae.S.

THE primary duties of an aircraft design team are to design an aircraft capable of meeting a certain specification of performance and manoeuvrability with suitable flying…

Rotor Blade Motion in a Vertical Sharp‐Edged Gust: A Stud/ of the Dynamics of Helicopter Blade Flapping with a Method of Deriving Maximum Gust Deflexion

P.R. Payne

This paper extends the work of Parts I and II to forward flight conditions, and completes the work on gust clearances.

The Library Shelf

W.A.M.

This unusual book gives a combined account of three different branches of dynamics, dealing with particles, fluids and solid bodies. The preface explains the history of the course…

Simplified Numerical Integration: A Successive Approximation Difference‐table Method for the Solution of Differential Equations

G.L Shue

TO facilitate the solution of differential equations by approximation methods, the writer has developed a simplified method of numerical integration.

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

American Research Fellowship Award Dr G. N. Lance, B.Sc, Ph.D., has been selected by the Royal Society for the award of one of the first Research Fellowships set up by the…

Auxiliary Equipment

New Lockheed Hydraulic Pump A new engine‐driven hydraulic pump with a rated maximum working pressure of 3,000 lb./sq. in., and a rated minimum delivery of 5–12 gal./min. has been…

Month in the Patent Office

These abstracts of British Patent Specifications are condensed, by permission, from the official specifications. Copies of the full specifications are obtainable from the Patent…

U.S. Patent Specifications

These details and drawings of patents granted in the United States are taken, by permission of the Department of Commerce, from the ‘Official Gazette of the United States Patent…

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