Examples show that take-off distance of only 500 m is possible, even with aircraft of high wing loading and high power loading; it appears that large sums put aside for runway extensions in planning post war airports, should be used for development of aircraft on line shown in paper; increase in wing loading would lead to economic aircraft for long distances. English abstract from Flugwehr u Technik n 1, 2, Jan, Feb 1944 p 23-8. (see also Engrs' Digest (Brit Edition) v 5 n 10 Oct 1944 p 299-502; Engrs' Digest (Am Edition) v 1 n 12 Nov 1944 p 675-8)
Airscrew thrust and take-off
Aircraft Eng
Aircraft Engineering ; 16 , n 187
1944
5 pages
Bibliography
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1944
|Emerald Group Publishing | 1944
|Engineering Index Backfile | 1944
|Static thrust of lifting airscrew
Engineering Index Backfile | 1937
|Static thrust of lifting airscrew
Engineering Index Backfile | 1937
|