Hostname: page-component-78c5997874-lj6df Total loading time: 0 Render date: 2024-11-09T15:45:46.264Z Has data issue: false hasContentIssue false
  • English
  • Français

Some Aerodynamic Aspects of Rear Mounted Engines*

Published online by Cambridge University Press:  04 July 2016

G. M. Moss
G. M. Moss*
Affiliation:
Applied Mechanics Branch, Royal Military College of Science
Get access Rights & Permissions [Opens in a new window]

Extract

The advent of a new generation of turbojet powered transport aircraft with engines mounted on the rear fuselage has complicated the task of the aerodynamicist, particularly when an attempt is made to determine the individual contributions to the stability and aerodynamic loading of the aircraft. This paper gives some idea of the additional complexity which is directly attributable to the presence of these engine nacelles and their effects on manoeuvring tail loads. Where rational methods are available for determining these effects they are referred to or included.

Type
N. E. Rowe Medal Paper
Information
The Aeronautical Journal , Volume 68 , Issue 648 , December 1964 , pp. 837 - 842
Copyright
Copyright © Royal Aeronautical Society 1964

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.)

Footnotes

*

Joint Award 21-26 Years of Age Group Luton Branch.

References

1.Lambert, D. J. The Design of Modern Pure Jet Transport Aircraft with Rear Mounted Engines Reviewed from Engineer ing and Operational Aspects. IAS National Summer Meeting, June-July 1960.Google Scholar
2.Lambert, D. J. Specialized Design for the Short Haul Jet Transport Role. S.A.E. Preprint 512A.Google Scholar
3.Duncan, W. J.The Principles of the Control and Stability of Aircraft. Cambridge University Press, 1952.Google Scholar
4.Atchison, J. R. Method of Determining Reduction in Elevator Effectiveness When Engine is Mounted on Aft Fuselage of Aircraft. WADD TN 61-52.Google Scholar
5.Diederich, F. W. Charts and Tables for use in Calculations of Downwash of Wings of Arbitrary Planform. NACA TN 2353.Google Scholar
6.Moss, G. Nacelles. H.A.L. Aero M. Lift Curve Slope for Rear MountedNote 67.Google Scholar
7.Moss, G. M. Spanwise Load Distribution due to Incidence for Rear Mounted Nacelles. H.A.L. Aero Note 76.Google Scholar
8.Czaykowski, T. Loading Conditions of Tailed Aircraft in Longitudinal Manoeuvre. A.R.C. R & M 3001.Google Scholar
9. Pilot Induced Pitching Manoeuvres. B.C.A.R. Paper No. 299.Google Scholar