Hostname: page-component-78c5997874-mlc7c Total loading time: 0 Render date: 2024-11-19T15:46:16.913Z Has data issue: false hasContentIssue false
  • English
  • Français

Multi-disciplinary simulation of propeller-turboprop aircraft flight

Published online by Cambridge University Press:  27 January 2016

A. Filippone  and
Z. Mohamed-Kassim
A. Filippone*
Affiliation:
School of Mechanical, Aerospace & Civil Engineering, University of Manchester, Manchester, UK
Z. Mohamed-Kassim
Affiliation:
School of Mechanical, Aerospace & Civil Engineering, University of Manchester, Manchester, UK
*
a.filippone@manchester.ac.uk
Get access Rights & Permissions [Opens in a new window]

Abstract

This contribution presents a novel simulation for a fixed-wing aircraft powered by gas turbine engines and advanced propellers (turboprops). The work is part of a large framework for the simulation of aircraft flight through a multi-disciplinary approach. Novel numerical methods are presented for flight mechanics, turboprop engine simulation (in direct and inverse mode), and propeller dynamics. We present in detail the integration of the propeller with the airframe, aircraft and tonal noise model. At the basic level, we address a shortfall in multi-disciplinary integration in turboprop-powered aircraft, including economical operations and environmental emissions (exhausts and noise). The models introduced are based on first principles, supplied with semi-empirical correlations, if required. Validation strategies are presented for component-level analysis and system integration. Results are presented for aerodynamics, specific air range, optimal cruise conditions, payload-range performance, and propeller noise. Selected results are shown for the ATR 72-500, powered by PW127M turboprop engines and F568-1 propellers.

Type
Research Article
Information
The Aeronautical Journal , Volume 116 , Issue 1184 , October 2012 , pp. 985 - 1014
Copyright
Copyright © Royal Aeronautical Society 2012 

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. Filippone, A. Comprehensive analysis of transport aircraft flight performance, Prog Aerospace Sci, April 2007, 43, (3), pp 192–236.Google Scholar
2. Filippone, A. Theoretical framework for the simulation of transport aircraft flight, J Aircr, 2010, in press.Google Scholar
3. Filippone, A. Analysis of carbon-dioxide emissions from transport aircraft, J Aircr, January 2008, 45, (1), pp 183–195.Google Scholar
4. Filippone, A. Steep-descent manoeuvre of transport aircraft, J Aircr, September 2007, 44, (5), pp 1727–1739.Google Scholar
5. Visser, W.J.P. and Broomhead, M.J. GSP: A generic object-oriented gas turbine simulation environment, 2000, ASME 2000-GT-0002, ASME Gas Turbine Conference, Munich, Germany. Program available from www.gspteam.com.Google Scholar
6. Filippone, A. Rapid estimation of airfoil aerodynamics for helicopter rotor calculations, J Aircr, 45, (4), pp 1468–1472.Google Scholar
7. Adkins, C.N. and Liebeck, R.H. Design of optimum propellers, J Propulsion & Power, July 2008, 10, (5), pp 676–682, September 1994.Google Scholar
8. Vincenty, M. Direct and inverse solutions of geodesics on the ellipsoid with application of nested equations, 1975, Technical Report XXIII, No 176, Survey Review.Google Scholar
9. Heidmann, M.F. Interim prediction method for fan and compressor noise source, 1975, Technical Report TM X-71763, NASA.Google Scholar
10. ESDU. Prediction of combustor noise from gas turbine engines, February 2005, Data Item 05001, ESDU International, London, UK.Google Scholar
11. Zorumski, W.E. Aircraft noise prediction program (ANOPP) theoretical manual, February 1982,, NASA Technical Report TM-83199, Part 2.Google Scholar
12. Fisher, M.J., Preston, G.A. and Bryce, W.D. A modelling of the noise from coaxial jets. Part 1: With unheated primary flow, J Sound & Vibration, January 1998, 209, (3), pp 385–403.Google Scholar
13. Fisher, M.J., Preston, G.A. and Mead, W.D. A modelling of the noise from coaxial jets. Part 2: With heated primary flow, J Sound & Vibration, January 1998, 209, (3), pp 405–417.Google Scholar
14. Simonich, J., Amiet, R., Schlinker, R. and Greizer, E. Helicopter rotor noise due to ingestion of atmospheric turbulence, May 1986, NASA Technical Report CR-3973.Google Scholar
15. Gerhold, C.H. Analytical model of jet shielding, AIAA J, May 1983, 21, (5), pp 694–698.Google Scholar
16. Lilley, G.M. The prediction of airframe noise and comparison with experiment, J Sound & Vibration, 2001, 239, (4), pp 849–859.Google Scholar
17. ESDU. Airframe Noise Prediction, June 2003, Data Item 90023, ESDU International, London, UK.Google Scholar
18. Humphreys, W.M. and Brooks, T.F. Noise spectra and directivity for a scale-model landing gear, AIAA 2007-3458, May 2007, 13th AIAA/CEAS Aeroacoustics Conference, Rome, Italy.Google Scholar
19. Guo, Y.P. A component-based model for aircraft landing gear noise prediction, J Sound & Vibration, 2008, 312, pp 801–820.Google Scholar
20. Anon, . Method for the calculation of the absorption of sound by the atmosphere, June 1978, Technical Report S1.26-1978, American National Standards Institute.Google Scholar
21. Rasmussen, K.B. Sound propagation over grass covered ground, J Sound & Vibration, 1981, 78, (2), pp 247–255.Google Scholar
22. Attenborough, K. Ground parameter information for propagation modeling, J Acoust Soc Am, January 1992, 92, (1), pp 418–427.Google Scholar
23. Hanson, D.B. and Parzych, D.J. Theory for noise of propellers in angular inflow with parametric studies and experimental verification, March 1993, NASA Technical Report CR-4499.Google Scholar
24. Caldarelli, G. ATR-72 accident in Taiwan, October 2007, SAE Aircraft & Engine Icing International Conference, ICE 13, Sevilla, Spain.Google Scholar