Hostname: page-component-cd9895bd7-q99xh Total loading time: 0 Render date: 2024-12-26T05:15:15.806Z Has data issue: false hasContentIssue false

Control Beyond the Stall

Published online by Cambridge University Press:  28 July 2016

Extract

The following paper does not pretend to be a complete and exhaustive survey of all the theoretical and experimental work which has been done up to the present on the subject of control beyond the stall.

It is confined to main questions and to a report of the practical research work upon which my colleagues and I have been engaged during the last two years.

In doing so I am well aware of the incompleteness of our research work and its methods, which aimed more at finding ad hoc than general solutions. The outlook of the engineer is different from that of the learned scientist. Not for him is the tranquil and contemplative atmosphere that surrounds purely scientific research work. If he breaks new ground he has neither time nor means to strive for a thorough, complete and general treatment of the particular problem he encounters. His work is limited by financial considerations; hampered by a rigid system of Works Orders; and by the lesser interest in so-called “unproductive” work which characterises industrial institutions. In short, from his point of view, the solution is infinitely more important than the theory or the methods by which it is obtained. A practical solution often presents itself automatically if the physical conditions of a particular problem are properly recognised, even if the degree of accuracy does not satisfy the rigid requirements of pure scientific research.

Type
Proceedings
Copyright
Copyright © Royal Aeronautical Society 1932

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

1. “The Lateral Control of Stalled Aeroplanes.” General Report by the Stability and Control Panel. R. & M. No. 1000, page 2.Google Scholar
2. (a) “The Longitudinal Control of an Aeroplane beyond the Stall,” by Garner, H. M., M.A., and Wright, K. V., B.A. R. & M. No. 1193.Google Scholar
2. (b) “Notes on Longitudinal Stability at Stalling in Gliding Flight,” by Gates, S. B., M.A. R. & M. No. 1189.Google Scholar
2. (c) “Longitudinal Control and Stability when Stalled,” by Jones, F. T. and Alston, R. P.. R. & M. No. B67.Google Scholar
2. (d) “Beitrag zur Entwickelung eines autorotationsfreien steil landbaren Flugzeuges,” von Wilhelm Schmidt, Dr.-Ing. Dissertation of the T.H. Berlin, 1930. Also published in Z.F.M., 1931, page 576 and following.Google Scholar
3. “Das gefährliche seitliche Kippen eines Flugzeuges über den Flügel und seine Beeinflussung,” von Richard Fuchs und Wilhelm Schmidt. Z.F.M., 1931, page 393.Google Scholar
4. “Step-by-step calculations upon the asymmetric movements of stalled aeroplanes,” by ProfessorJones, B. M., M.A., A.F.C., and MissTrevelyan, A., B.Sc. R. & M. No. 999.Google Scholar
5. “Rolling and sideslip experiments on a model slotted biplane of R.A.F. 31 section,” by Irving, H. B., B.Sc, Batson, A. S., B.Sc., and Maidens, A. L.. R. & M. No. 1240.Google Scholar
6. “The Choice of a Wing Section,” by Dr.Munk, Max. “Aero Digest,” September, 1931, page 47.Google Scholar
7. “Flight tests on an Atlas fitted with Automatic Slots connected with the Ailerons,” by Jones, E. T.. R. & M. No. 1260.Google Scholar
8. “Full-scale Determination of the motions, at the stall, of a Bristol Fighter aeroplane fitted with autocontrol slots and interceptors,” by Ormerod, A., B.Sc. Report No. B.A. 916.Google Scholar
9. “Full-scale control tests on a Fokker F.VII.-3M Monoplane.”Google Scholar
10. “Luftkräfte und Luftkraftmomente bei grossen Anstellwinkeln und ihre Abhängigkeit von der Tragwerksgestalt,” von Richard Fuchs und Wilhelm Schmidt. Z.F.M., 1930. Helt 1.Google Scholar
11. “Fine Möglichkeit zur Unterdrückung der Autorotation von Tragflächen,” Schrenk, von O.. Z.F.M., 1929. Heft 21.Google Scholar
12. “Tests of various lateral controls fitted to a Sisken Aircraft,” by Jennings, W. G., B.Sc. R. & M. 1384.Google Scholar
13.Applied Aerodynamics,” by Bairstow, L., 1920. (Longmans, Green & Co.)Google Scholar
14. “Abwindmessungen hinter Tragflügeln mit abgerissener Strömung,” Petersohn, von E.. Z.F.M., page 289.Google Scholar
15. “Contribution à l'étude experimental du champ aérodynamique autour d'un profil sustentateur,” A. Lapresle. Bulletin Technique, November, 1927. Service technique et industriel de 1'aéronautique.Google Scholar
16. “On the theory of tapered aerofoils,” by Fage, A., A.R.C.Sc. R. & M. No. 806.Google Scholar