Hostname: page-component-77c89778f8-n9wrp Total loading time: 0 Render date: 2024-07-20T06:10:41.677Z Has data issue: false hasContentIssue false
  • English
  • Français

Free Flight Techniques for High Speed Aerodynamic Research

Published online by Cambridge University Press:  28 July 2016

J. A. Hamilton  and
P. A. Hufton
J. A. Hamilton
Affiliation:
Royal Aircraft Establishment, Farnborough
P. A. Hufton
Affiliation:
Royal Aircraft Establishment, Farnborough
Get access Rights & Permissions [Opens in a new window]

Extract

The 969th Lecture to be given before the Society and the 22nd Main Lecture to be held at a Branch Centre, “ Free Flight Techniques for High Speed Aerodynamic Research ” by J. A. Hamilton, M.B.E., B.Sc, A.M.I.Mech.E., A.F.R.Ae.S., and P. A. Hufton, M.Sc, was given under the auspices of the Boscombe Down Branch on 1st December 1955. Air Commodore R. A. Ramsay Rae, O.B.E., President of the Branch welcomed the guests and said how delighted he was to see the President of the Society, Mr. N. E. Rowe and members of the Council and Main Society at the Aeroplane and Armament Experimental Establishment.

Type
Research Article
Information
The Aeronautical Journal , Volume 60 , Issue 543 , March 1956 , pp. 151 - 185
Copyright
Copyright © Royal Aeronautical Society 1956

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. Staff of the Supersonics Division, Royal Aircraft Establishment (1950). Flight Trials of a Rocket-Propelled Transonic Research Model: The R.A.E. Vickers Rocket Model. Parts I to IV. R. & M. No. 2835, 1954.Google Scholar
2. Kell, C. (Editor) (1952). Flight Tests at Transonic Speeds on Freely Falling Models. Parts I to V. R. & M. No. 2902, 1955.Google Scholar
3. Holder, D. W., Pearcey, H. H. and Gadd, G. E. (1954). The Interaction Between Shock Waves and Boundary Layers. C.P. No. 180, 1955.Google Scholar
4. Gates, S. B. and Lyon, H. M. (1944). A Continuation of Longitudinal Stability and Control Analysis. Part I. General Theory. R. & M. No. 2027, 1947.Google Scholar
5. Broadbent, E. G. (1950). The Rolling Power of an Elastic Swept Wing. R. & M. No. 2857, 1954.Google Scholar
6. Voepel, H. M. A. (1955). The Influence of Acceleration on the Short-Period Longitudinal Oscillation of an Aircraft. Unpublished R.A.E. Report.Google Scholar
7. De Young, J. (1950). Theoretical Antisymmetric Span Loading for Wings of Arbitrary Planform at Subsonic Speeds. N.A.C.A. Report No. 1056, 1951.Google Scholar
8. Brown, C. E. and Adams, M. C. (1948). Damping in Pitch and Roll of Triangular Wings at Supersonic Speeds. N.A.C.A. Report No. 892, 1948.Google Scholar
9. Malvestuto, F. S., Margolis, K. and Ribner, H. S. (1949). Theoretical Lift and Damping in Pitch of Thin Sweptback Wings of Arbitrary Taper and Sweep at Supersonic Speeds (Subsonic Leading Edges and Supersonic Trailing Edges). N.A.C.A. Technical Note No. 1860, 1949.Google Scholar
10. Harmon, S. M. and Jeffreys, I. (1950). Theoretical Lift and Damping in Roll of Thin Wings with Arbitrary Sweep and Taper at Supersonic Speeds. (Supersonic Leading and Trailing Edges.) N.A.C.A. Technical Note No. 2114, 1950.Google Scholar
11. Ribner, H. S. (1950). On the Effect of Subsonic Trailing Edges in the Damping in Roll and Pitch of Thin Sweptback Wings in a Supersonic Stream. N.A.C.A. Technical Note No. 2146, 1950.Google Scholar