Aircraft Engineering and Aerospace Technology: Volume 25 Issue 11
Strapline:
An International JournalTable of contents
Deliberations on Documentation
WE have received the Summary Records of the first two meetings of the Documentation Committee of the Advisory Group for Aeronautical Research and Development (AGARD) of the North…
Structural Aspects of Swept‐Back Wings: An Account of Research Work in Sweden, with Particular Reference To Model Tests
B.R. NotonTHE efficient design and construction of the latest types of Swedish military aircraft, with wings with high critical Mach numbers, has necessitated a thorough investigation into…
A Method of Estimating Helicopter Performance: The Calculation of an Estimated Performance at the Project Stage
P.R. PayneBased fundamentally on the ‘Energy Method’ approach to helicopter performance calculation, a method is presented for calculating performance of a design in the project stage. In…
A New Electronic Analogue Computer: A Compact General‐Purpose Instrument Designed for Quantity Production
E. Lloyd ThomasTHE increasing necessity for large‐scale calculation in the design of aircraft has, in recent years, emphasized the lack of adequate computational facilities and transferred…
Research Reports and Memoranda
Under this heading are published regularly abstracts of all Reports and Memoranda or the Aeronautical Research Council, Reports and Technical Memoranda of the United States…
Trade Announcements
Auto Diesels Ltd. Auto Diesels Ltd., Uxbridge, have announced the appointment to the Board of Directors of Air Commodore James Warburton, who will be mainly concerned with their…
Month in the Patent Office
An aircraft fitted with fixed wings 14 and a conventional empennage 12, which would be ineffective with the machine hovering or moving forward at very low speed, is rendered…
U.S. Patent Specifications
An aeroplane which comprises, in combination, a wing with two spans, a fuselage centrally of said spans, and bracing struts connected to the fuselage and to points on the wing…
ISSN:
0002-2667Online date, start – end:
1929Copyright Holder:
Emerald Publishing LimitedOpen Access:
hybridEditor:
- Prof Phil Webb