Introduction to Aircraft Aeroelasticity and Loads: Second Edition

Introduction to Aircraft Aeroelasticity and Loads: Second Edition

Volumn , Issue , 2015, Pages 1-543

  Wright, Jan R ^a,b   Cooper, Jonathan E ^c  

^a UNIVERSITY OF MANCHESTER   (United Kingdom)

^b J2W Consulting   (United Kingdom)

^c UNIVERSITY OF BRISTOL   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT; ELASTIC WAVES; MATLAB; STUDENTS; TEXTBOOKS;

AEROELASTIC BEHAVIOUR; AEROELASTIC MODELING; AIRCRAFT RESPONSE; CERTIFICATION REQUIREMENTS; FLEXIBLE AIRCRAFT; GRADUATE STUDENTS; LECTURE SLIDES; THEORETICAL APPROACH;

AEROELASTICITY;

EID: 85015162323     PISSN: None     EISSN: None     Source Type: Book    
DOI: 10.1002/9781118700440     Document Type: Book

References (32)

1. Advisory Group for Aerospace Research and Development (AGARD) Manual of Aeroelasticity 1956-1970, NATO (North Atlantic Treaty Organization), Brussels.
2. Albano, E. and Rodden, W.P. (1969) A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows. AIAA Journal, 7 (2), 279-285.
3. Anderson, A. (2001) Fundamentals of Aerodynamics, 3rd edn, McGraw-Hill, New York.
4. Babister, A.W. (1980) Aircraft Dynamic Stability and Response, Pergamon Press, Oxford.
5. Bairstow, L. and Fage, A. (1916) Oscillations of the Tailplane and Body of an Aircraft in Flight. ARC R&M (Aeronautical Research Council Reports and Memoranda) 276, part 2AERADE Reports Archive, Cranfield.
6. Benham, P.P., Crawford, R.J. and Armstrong, C.G. (1996) Mechanics of Engineering Materials, 2nd edn, Longman, London.
7. Bishop, R.E.D. and Johnson, D.C. (1979) The Mechanics of Vibration, Cambridge University Press, Cambridge.
8. Bisplinghoff, R.L., Ashley, H. and Halfman, R.L. (1996) Aeroelasticity, Dover (Addison Wesley, 1955), New York.
9. Blair, M. (1994) A Compilation of the Mathematics Leading to the Doublet Lattice Method. WL-TR-95-3022.
10. Blevins, R.D. (2001) Formulas for Natural Frequency and Mode Shape, Kreiger, Malabar, FL, USA.
11. Broadbent, E.G. (1954) The elementary theory of aeroelasticity. Aircraft Engineering and Aerospace Technology, 26 (3), 70-79.
12. Bryan, G.H. (1911) Stability in Aviation, Macmillan, London.
13. Chen, P.C. (2000) A damping perturbation method for flutter solution: the g-method. AIAA Journal, 38 (9), 1519-1524.
14. Collar, A.R. (1978) The first fifty years of aeroelasticity. Aerospace, 5 (2), 12-20.
15. Collar, A.R. and Simpson, A. (1987) Matrices and Engineering Dynamics, Ellis Horwood, Harlow.
16. Cook, M.V. (1997) Flight Dynamics Principles, Arnold, London.
17. Cook, R.D., Malkus, D.S. and Plesha, M.E. (1989) Concepts and Applications of Finite Element Analysis, John Wiley & Sons, Ltd., Chichester, UK.
18. Cooper, J.E., Lind R. and Wright, J.R. (2010) Aeroelastic Testing and Certification Encyclopedia of Aerospace Engineering. John Wiley & Sons, Ltd, Chichester, UK.
19. Craig, R.R. and Kurdila, A.J. (2006) Fundamentals of Structural Dynamics, John Wiley & Sons, Ltd, Chichester, UK.
20. CS-25: Certification Specifications for EASA (European Aviation Safety Agency); http://www.easa. europa.eu
21. Theodorsen, T. (1935) General Theory of Aerodynamic Instability and the Mechanism of Flutter. National Advisory Committee for Aeronautics NACA Report 496, AERADE Reports Archive, Cranfield, UK.
22. Thomson, W.T. (1997) Theory of Vibration with Applications, 5th edn, Chapman and Hall, London.
23. Tse, F.S., Morse, I.E. and Hinkle, R.T. (1978) Mechanical Vibrations: Theory and Applications, Allyn and Bacon, Boston, MA, USA.
24. Waszak, M.R. and Schmidt, D.K. (1988) Flight dynamics of aeroelastic vehicles. Journal of Aircraft, 25 (6), 563-571.
25. Weisshaar, T.A. (2010) Static and Dynamic Aeroelasticity. Encyclopedia of Aerospace Engineering, John Wiley & Sons, Ltd, Chichester, UK.
26. Wells, D.A. (1967) Theory and Problems of Lagrangian Dynamics, Schaum'sOutline Series,McGraw-Hill, New York.
27. Whittle, P. (1996) Optimal Control, Basics and Beyond, John Wiley & Sons Ltd, Chichester, UK.
28. Wright, J.R., Wong, J., Cooper, J.E. et al. (2003) On the use of control surface excitation in flutter testing, Proc. Instn Mech. Engrs, Part G: J. Aerospace Engineering, 217 (96), 317-332.
29. Yates, E.C. (1966) Modified strip analysis method for predicting wing flutter at subsonic to hypersonic speeds. Journal of Aircraft, 3 (1), 25-29.
30. Young, W.C. (1989) Roark's Formulas for Stress and Strain, 6th edn, McGraw-Hill, New York.
31. Zimmermann, H. (1991) Aeroservoelasticity. Computer Methods in Applied Mechanics and Engineering, 90 (13), 719-735.
32. Zimmermann, N.H. and Weissenberger, J.T. (1964) Prediction of flutter onset speed based on flight testing at subcritical speeds. Journal of Aircraft, 1 (4), 190-202.