Hostname: page-component-586b7cd67f-2plfb Total loading time: 0 Render date: 2024-11-25T07:12:30.892Z Has data issue: false hasContentIssue false
  • English
  • Français

The Effect of Wing Loading on the Design of Modern Aircraft with Particular Regard to the Take-Off Problem

Published online by Cambridge University Press:  28 July 2016

H. F. Vessey
Get access Rights & Permissions [Opens in a new window]

Extract

The author wishes to express his appreciation of the honour that has been paid him in being requested to present a paper before the Royal Aeronautical Society. Permission has been given by the Air Ministry for the publication of the paper, but the author is alone responsible for the views expressed.

Type
Proceedings
Information
The Aeronautical Journal , Volume 42 , Issue 329 , May 1938 , pp. 369 - 404
Copyright
Copyright © Royal Aeronautical Society 1938

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

page 374 note * Journal of the Royal Aeronautical Society, August, 1935.

page 377 note * Handbook of Aeronautics, Part II, page 176.

page 378 note * Journal of the Royal Aeronautical Society, November, 1935.

page 384 note * N.A.C.A. Report No. 583. “The Rolling Friction of several Aeroplane Wheels and Tires,” by J. W. Wetmore.

page 391 note * N.A.C.A. Technical Note No. 557.

page 395 note * Lachmann. “Skin friction from the point of view of the Aeronautical Engineer.” Cambridge University Engineering and Aeronautical Society’s Journal, 1937.

page 408 note * “Aircraft Performance Estimation” by C. O. Vernon, Student. J.R. Ae. Soc., Aug., 1937.