Hostname: page-component-586b7cd67f-tf8b9 Total loading time: 0 Render date: 2024-11-24T21:50:21.000Z Has data issue: false hasContentIssue false
  • English
  • Français

Part 1 — Introduction to the concept of axiomatic aerodynamic modelling

Published online by Cambridge University Press:  04 July 2016

G. J. Hancock  and
J. S. Y. Lam
G. J. Hancock
Affiliation:
Department of Aeronautical Engineering Queen Mary College, University of London
J. S. Y. Lam
Affiliation:
Department of Aeronautical Engineering Queen Mary College, University of London
Get access Rights & Permissions [Opens in a new window]

Summary

The aim of axiomatic aerodynamic modelling is introduced, namely to understand the validity of aerodynamic modelling in the context of aircraft dynamics with particular emphasis on understanding the relationship between full-scale flight behaviour as compared with that predicted from data based on wind tunnel tests.

Type
On the application of axiomatic aerodynamic modelling to aircraft dynamics
Information
The Aeronautical Journal , Volume 91 , Issue 901 , January 1987 , pp. 1 - 3
Copyright
Copyright © Royal Aeronautical Society 1987 

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. Orlik Ruckemann, K. Review of techniques for determination of dynamic stability parameters in wind tunnels. AGARD Lecture Series No 114, 1981.Google Scholar
2. Tobak, H. and Schiff, L. Aerodynamic mathematical modelling — basic concepts. AGARD Lecture Series No 114, 1981.Google Scholar
3. Thomas, H. H. B. M. Some thoughts on mathematical models for flight dynamics. The Aeronautical Journal, May 1984, 88, 875, 169–178.Google Scholar
4. Katz, J. and Schiff, L. B. Modelling aerodynamic responses to aircraft manoeuvres — a numerical validation. J Aircraft, January 1986, 23, 19–25.Google Scholar