Aircraft Engineering and Aerospace Technology: Volume 9 Issue 11
Strapline:
An International JournalTable of contents
The Stalling of Tapered Wings: Puzzling Results with Two Junkers Wings of Different Plan
WE are greatly indebted to MR. SHENSTONE for calling attention to the paper, published in the 1936 year book of the Lilienthal‐Gesellschaft für Luftfahrtforschung, by HERR QUICK…
The Modern Junkers Wing: The Aerodynamic Development of the JU 86 Wing with Particular Reference to Lateral Stability
A.W. QuickIF I am to cover the development of the Ju 86 wing in this short paper, it will be obvious that I shall not be able to touch upon all the aerodynamic problems encountered. Thus I…
Balancing of Flaps: Aerodynamic and Mechanical Methods of Reducing the Effort Required
J.E. SerbyTRAILING edge flaps, it seems, have come to stay for some time; the devices that looked almost too good to be true when first investigated have proved invaluable, not only as aids…
Hydraulic Pumps for Aeroplanes: A Survey of the Types Available for the Operation of Auxiliary Services
Frank NixonTHE past two years have seen a notable increase in the number of services on aircraft for which some form of power is required. First, retractable undercarriages, followed by wing…
Air Ministry Contracts
THE following list of contracts placed by the Air Ministry during August is extracted from the September issue of The ministry of Labour Gazette:
Research Reports and Memoranda
Under this heading are published regularly abstracts of all Reports and Memoranda of the Aeronautical Research Committee, Reports and Technical Notes of the U.S. National Advisory…
Combined Stresses: Working Charts for Combined Stress Factors and Selection of Suitable Members
H. ParkinsonIn all drawing offices “labour‐saving” methods of making approximate preliminary calculations are in use. Here the author renders useful service in throwing open to others charts…
U.S. Patent Specifications
In a hub for airplane or similar propellers having a plurality of blades, sleeves integral with the hub adapted to receive the spindles of the blades so as to permit their turning…
Month in the Patent Office
Aircraft control surfaces 3, Fig. 1, are pivotally attached about forwardly convergent axes to wing or tailplane 2 and are arranged to constitute overlapping tips thereto and are…
ISSN:
0002-2667Online date, start – end:
1929Copyright Holder:
Emerald Publishing LimitedOpen Access:
hybridEditor:
- Prof Phil Webb