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Handling Criteria

Published online by Cambridge University Press:  04 July 2016

F. O'hara*
Affiliation:
Royal Aircraft Establishment, Bedford

Summary

The nature of handling criteria and their uses in relation to the prediction of aircraft handling characteristics are discussed. A brief history is given of the development of ideas on handling, and a survey is made of criteria for modern aircraft, looking particularly at the physical factors affecting the pilot, as an indication of the basis of the criteria. The novel handling features arising with new aircraft species like slender wings and VTOL are considered. The scope of flight simulators and variable stability aircraft for systematic study of handling is discussed and the potentialities of theoretical study by means of servo analysis techniques considered. Finally, possible lines of development in relation to the assessment of aircraft handling characteristics are suggested.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1967

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References

1.Bairstow, L.. Melvill Jones, B. and Thompson, A. W. H. Investigation into the Stability of an Aeroplane. R and M 77, March 1913.Google Scholar
2.Rayleigh, . Lord. Report of the Advisory Committee for Aeronautics for 1912-13.Google Scholar
3.Gates, S. B. and Bryant, L. W. The Spinning of Aeroplanes. R and M 1001. October 1926. Google Scholar
4.Gates, S. B. An Analysis of Static Longitudinal Stability in relation to Trim and Control Force. R and M 2132, April 1939.Google Scholar
5.Gates, S. B. and Lyon, H. M. A Continuation of Longitudinal Stability and Control Analyses. R and M 2027, February 1944.Google Scholar
6.Gilruth, R. R. Requirements for Satisfactory Flying Qualities of Airplanes. NASA Report No. 755, 1943.Google Scholar
7.Cooper, G. E. Understanding and Interpreting Pilot Opinion. Aero Eng Review, March 1957.Google Scholar
8.Duncan, W. J.The Principles of the Control and Stability of Aircraft. Cambridge University Press, 1952.Google Scholar
9.Newell, F. and Rhoads, D. W. Flight Evaluations of the Effect of Variable Phugoid Damping in a JTB-26B Airplane. Cornell Aero Lab WADC TR 56-223, Dec 1956. Google Scholar
10.Bisgood, P. L. A Review of Recent Handling Qualities Research—Longitudinal Aspects. Unpublished RAE Report.Google Scholar
11.Leyman, C. A Survey of Aircraft Handling Criteria. BAC (Filton) Aerodynamics Note No. 128, Dec 1964.Google Scholar
12.Lean, D. and Eaton, R. The Influence of Drag Characteristics on the Choice of Landing Approach Speeds. AGARD Report 122, May 1957.Google Scholar
13.Staples, K. J. Flight Measurements of the Influence of Speed Stability on the Landing Approach. AGARD Report 420, January 1963.Google Scholar
14.Perry, D. H. Flight Simulators and the Study of Aircraft Handling Characteristics. Unpublished RAE Report.Google Scholar
15.Newell, F. and Campbell, G. Flight Evaluations of Variable Short-Period and Phueoid Characteristics in a B26. Cornell Aero Lab Inc WADC TR 54-594, Dec 1954.Google Scholar
16.Kolk, W. R.Modern Flight Dynamics. Prentice-Hall International, Inc. 1961.Google Scholar
17.Chalk, C. R. Fixed-Base Simulator Investigation of the Effects of L and True Speed on Pilot Opinion of Longitudinal Flying Qualities. Cornell Aero Lab ASD-TD R-63-399, November 1963.Google Scholar
18.Harper, R. P. Jr. Flight Evaluations of Various Longitudinal Handling Qualities in a Variable Stability Jet Fighter. Cornell Aero Lab WADC TR-55-299, July 1955.Google Scholar
19.McFadden, N. M., Vomaske, R. F. and Heinle, D. R. A Flight Investigation using Variable Stability Airplanes of Minimum Stability Requirements for High Speed, High Altitude Vehicles. NASA TN D779.Google Scholar
20.Creer, B. Y., Stewart, J. D., Merrick, R. B. and Drinkwater, F. J. A Pilot Opinion Study of Lateral Control Requirements for Fighter-Type Aircraft. NASA Memo 1-29-59A, March 1959.Google Scholar
21.Bisgood, P. L. A Review of Recent Handling Qualities Research and its Application to the Handling Problems of Large Aircraft: Lateral Directional Aspects. RAE Report Aero 2688, June 1964.Google Scholar
22.Perry, D. H., Port, W. G. A. and Morrall, J. C. A Flight Study of the Sidestep Manoeuvre during Landing. R and M 3347, July 1961.Google Scholar
23.Pinsker, W. J. G. Features of Large Transport Aircraft affecting Control during Approach and Landing. AGARD Report 421, January 1963.Google Scholar
24. Recommendations for V/STOL Handling Qualities. AGARD Report 408. October 1962.Google Scholar
25.Perry, D. H. and Chinn, H. W. A Preliminary Flight Simulation Study of Jet-Borne VTOL Aircraft Handling Qualities. Unpublished RAE Report.Google Scholar
26.Lynn, R. B. New Control Criteria for VTOL Aircraft. Aerospace Engineering, August 1962.Google Scholar
27.Chinn, H. W. Results of Flight Tests on the Shorts SCI VTOL Research Aircraft with particular reference to Handling Qualities in the Hover and Transition. AGARD Report, September 1965.Google Scholar
28.Perry, D. H. and Naish, J. M. Flight Simulation for Research. Journal of the Royal Aeronautical Society, October 1964.Google Scholar
29.O'Hara, F.Prediction of Aircraft Flying Qualities by Flight Simulators and other Methods. Proc Inter Council of Aero Sciences. Macmillan and Co, 1965.Google Scholar
30.Westbrook, C. B. The Status and Future of Flying Qualities Requirements. AIAA Paper No. 65-313, July 1965.CrossRefGoogle Scholar
31.Krendel, E. S. and McRuer, D. T. A Servo-Mechanism Approach to Skill Development. J Franklin Institute, January 1960.Google Scholar
32.Hall, I. A. M. Study of the Human Pilot as a Servo Element. Journal Royal Aeronautical Society, June 1963.Google Scholar
33.Ashkenas, I. L. and McRuer, D. T. A Theory of Handling Qualities derived from Pilot-Vehicle System Considerations. Aerospace Engineering, February 1962Google Scholar