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An introductory guide to literature in aeroelasticity

Published online by Cambridge University Press:  04 July 2016

R. S. Battoo
R. S. Battoo*
Affiliation:
Cranfield College of AeronauticsCranfield University, UK
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Abstract

This paper is meant primarily for non-specialist readers who may not be familiar with aeroelasticity. The main objective is to direct the reader to some important texts and papers that have been published in the areas which embrace aeroelasticity, from which the reader may gain sufficient knowledge about the subject. Since aeroelasticity is a large field which requires considerable knowledge in several related areas newcomers can often be daunted by the subject. This is further compounded by the great amount of published material available. This paper will assist the reader to locate key publications and help identify major works which have been useful in studying the subject. A comprehensive list of references is included which will help to identify key subject areas, researchers, research establishments and publications for further study.

Type
Research Article
Information
The Aeronautical Journal , Volume 103 , Issue 1029 , November 1999 , pp. 511 - 518
Copyright
Copyright © Royal Aeronautical Society 1999 

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References

References

7.1 Aeroelasticity — (text) books

Non English texts

1.1 Scanlan, R.H. and Rosenbaum, R. Introduction to the Study of Aircraft Vibration and Flutter, Macmillan, New York, USA, 1951.Google Scholar
1.2 Fung, Y.C. Introduction to the Theory of Aeroelasticity, John Wiley and Sons, New York, USA, 1955.Google Scholar
1.3 Bisplinghoff, R.L., Ashley, H. and Halfman, R.L. Aeroelasticity, Addison-Wesley Publishing, Cambridge, Mass, USA, 1955.Google Scholar
1.4 Bisplinghoff, R.L. and Ashley, H. Principles of Aeroelasticity, John Wiley and Sons, New York, USA, 1962.Google Scholar
1.5 Dowell, E.H., Crawley, E.F., Curtis, H.C., Peters, D.A., Scanlan, R.H. and Sisto, F. A Modem Course in Aeroelasticity, Kluwer Academic Publishers, The Netherlands, 3rd revised edition, 1995.Google Scholar
1.6 Dowell, E.H. and Ilgamov, M. Studies in Nonlinear Aeroelasticity, Springer-Verlag, New York, USA, 1988.Google Scholar
1.7 Bielawa, R.L. Rotary Wing Structural Dynamics and Aeroelasticity, AIAA, Washington DC, USA, 1992.Google Scholar
1.8 Dowell, E.H. Aeroelasticity of Plates and Shells, Noordoff International, Leyden, 1975.Google Scholar
1.9 Frazer, R.A. Elementary Matrices and Some Applications to Dynamics and Differential Equations, 1946.Google Scholar
1.11 Johnson, W. Helicopter Theory, Princeton University Press, 1980.Google Scholar
1.12 Templeton, H. Massbalancing of Aircraft Control Surfaces, Chapman and Hall, London, UK, 1954.Google Scholar
1.13 Abramson, H.N. An Introduction to the Dynamics of Airplanes, Ronald Press, New York, USA, 1958.Google Scholar
1.14 Rodden, W.R. and Johnson, E.H. MSC/NASTRAN Aeroelasticity Analysis Users Guide, Version 68, The Macneal-Schwendler, Los Angeles, USA.Google Scholar
1.15 Stinton, D. The Anatomy ofthe Aeroplane,GJ. Foulis, 1966.Google Scholar
1.16 Forsching, H.W. Grundlagen der Aeroelsatik “Fundamentals of Aeroelasticity”, (In German), Springer-Verleg ISBN 3-540-06540-7 New York, USA, 1974.Google Scholar
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1.16 Forsching, H.W. Grundlagen der Aeroelsatik “Fundamentals of Aeroelasticity”, (In German), Springer-Verleg ISBN 3-540-06540-7 New York, USA, 1974.Google Scholar
1.17 Petre, A. Theory of Aeroelasticity, Vol I Statics, Vol II Dynamics. (In Romanian), Publishing House of the Academy of the Socialist Republic of Romania, Bucharest, 1966.Google Scholar

7.2 Classic references — aeroelasticity

2.1 Van schoor, M.C. and Von Flotow, A.H. Aeroelastic characteristics of a highly flexible aircraft, J Aircr, October 1990, 27, (10), pp 901–908.Google Scholar
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2.3 Duncan, W.J. The fundamentals of flutter, RAE Report No Aero 1920; Reports and Memoranda No 2417, November 1948; also in Aircraft Engineering, January and February 1945. 2.4 AGARD Manual on Aeroelasticity, Vols I-VII, AGARD (circa 1965).Google Scholar
2.5 Babister, A.W. Flutter and divergence of sweptback and swept forward wings, College of Aeronautics, Report No 39, June 1950.Google Scholar
2.6 Collar, A.R. Aeroelastic problems at high speed, J Royal Aero Soc, January 1947, 51, (433), pp 1–34.Google Scholar
2.7 Frazer, R.A. and Duncan, W.J. The flutter of aeroplane tails, 1930, ARC R&M 1237.Google Scholar
2.8 Frazer, R.A. The flutter of aeroplane wings, J Royal Aero Soc, June 1929, 33, (222), pp 407–454.Google Scholar
2.9 Frazer, R.A. and Duncan, W.J. The flutter of aeroplane wings, ARC R&M 1155, 1928.Google Scholar
2.10 Cox, H. Roxbee, and Pugsley, A.G. Theory of loss of lateral control due to wing twisting, ARC R&M 1506, October 1932.Google Scholar
2.11 Garrick, I.E. (Ed) Aerodynamic Flutter, AIAA, New York, USA, March 1969.Google Scholar
2.12 Friedmann, P.P. and Chang, J.C.I. (Eds) Aeroelasticity and fluid structure interaction problems, AD-Vol. 44, ASME 1994, ISBN 0-7918-1453-X.Google Scholar
2.13 Freberg, C.R. and Kemler, E.N. Aircraft Vibration and Flutter, John Wiley and Sons, 1944.Google Scholar
2.14 Loring, S.J. General approach to the flutter problem, SAE Transactions, August 1941, pp 345-355.Google Scholar
2.15 Lockspeiser, B. A simple approach to the wing flutter problem, J Royal Aero Soc, September 1933, 37, pp 783–792.Google Scholar
2.16 Broadbent, E.G. The elementary theory of aero-elasticity, divergence and reversal of control, Aircraft Engineering, March 1954, 26, (301), pp 70–79.Google Scholar
2.17 Broadbent, E.G. The elementary theory of aero-elasticity, wing flutter, Aircraft Engineering, April 1954, 26, (302), pp 113–121.Google Scholar
2.18 Broadbent, E.G. The elementary theory of aero-elasticity, flutter of control surfaces and tabs, Aircraft Engineering, May 1954, 26, (303), pp 145–153.Google Scholar
2.19 Broadbent, E.G. The elementary theory of aero-elasticity, guiding principles in flutter analysis, Aircraft Engineering, June 1954, 26, (304), pp 192–200.Google Scholar
2.20 Reissner, H. Neuere probleme aus der Flugzeugstatik, Z. fur Flugtechnik und Motorluftschiffahrt, April 1926,17, (7).Google Scholar

7.3 Aeroelasticity review papers

3.1 Collar, A.R. The expanding domain of aeroelasticity, J Royal Aero Soc, June 1946, 50, pp 613–636.Google Scholar
3.2 Collar, A.R. Aeroelasticity — retrospect and prospect, J Royal Aero Soc, January 1959, 63, pp 1–15.Google Scholar
3.3 Loewy, R.G. Review of rotary-wing V/STOL dynamic and aero-elastic problems, J Amer Heli Soc, July 1969, 14, (3), pp 3–23.Google Scholar
3.4 Friedmann, P.P. Recent trends in rotary wing aeroelasticity, Vertica, 1987,11, (1/2), pp 139–170.Google Scholar
3.5 Chopra, I. Perspectives in aero-mechanical stability of helicopter rotors, Vertica, 1990,14, (4), pp 457–508 Google Scholar
3.6 Zimmermann, H. The aeroelastic challenge of the Airbus family — Review and Prospects, International Forum of aeroelasticity and structural dynamics. 3-5 June 1991, Aachen, pp 1-11.Google Scholar
3.7 Done, G.T.S. Past and future progress in fixed wing and rotary wing aeroelasticity, International Forum of aeroelasticity and struc tural dynamics, August 1995, Manchester, pp 23.1-23.13.Google Scholar
3.8 Friedmann, P.P. The renaissance of aeroelasticity and its future, International Forum of aeroelasticity and structural dynamics, June 1997, Rome.Google Scholar
3.9 Ashley, H. Aeroelasticity, Applied Mechanics Review, February 1970, 23, pp 119–129.Google Scholar
3.10 Ashley, H. Update to aeroelasticity, Applied Mechanics Update, Steele, C.R. and Springer, G.S. (Eds), ASME, New York, USA, 1986, pp 117–125.Google Scholar
3.11 Fleeter, S. Aeroelasticity research for turbomachine applications, J Aircr, 1979,16, pp 330–338.Google Scholar
3.12 Garrick, I.E. Aeroelasticity — Frontiers and Beyond, J Aircr, September 1976,13, (9), pp 641–657.Google Scholar
3.13 Abramson, H.N. Hydroelasticity: A review of hydrofoil flutter, Applied Mechanics Review, February 1969.Google Scholar
3.14 Garrick, I.E. and Reed, W.H. Historical development of aircraft flutter, J Aircr, November 1981,18, (11), pp 897–912.Google Scholar
3.15 Noor, A.K. and Venneri, S.L (Eds) Flight-Vehicle Materials, Structures and Dynamics — Assessment and Future Direction, Vol 5 Structural Dynamics and Aeroelasticity, New York, USA, ASME, 1993.Google Scholar
3.16 Bendiksen, O.O. Aeroelastic problems in turbomachines, Flight-Vehicle Materials, Structures and Dynamics — Assessment and Future Direction, Vol 5 Structural Dynamics and Aeroelasticity, New York, USA, ASME, 1993, Ch 3, pp 241–297.Google Scholar
3.17 Ricketts, R.H. Experimental aeroelasticity in wind tunnels — history, status and future in brief, Flight-Vehicle Materials, Structures and Dynamics — Assessment and Future Direction, Vol 5 Structural Dynamics and Aeroelasticity, New York, USA, ASME, 1993, Ch 2, pp 151–177.Google Scholar
3.18 Dowell, E.H. Nonlinear aeroelasticity, Flight-Vehicle Materials, Structures and Dynamics — Assessment and Future Direction, Vol 5 Structural Dynamics and Aeroelasticity, New York, USA, ASME, 1993, Ch 4, pp 213-239.Google Scholar
3.19 Edwards, J.W. Computational aeroelasticity, Flight-Vehicle Materials, Structures and Dynamics — Assessment and Future Direction, Vol 5 Structural Dynamics and Aeroelasticity, New York, USA, ASME, 1993, Ch 7, pp 393–436.Google Scholar
3.20 Friedmann, P.P. and Hodges, D.A. Rotary wing aeroelasticity with application to VSTOL vehicles. Flight-Vehicle Materials, Structures and Dynamics — Assessment and Future Direction, Vol 5 Structural Dynamics and Aeroelasticity, New York, USA, ASME, 1993, Ch 6, pp 299–391.Google Scholar
3.21 Harris, T.M., Noll, T.E., Hertz, T.J. and Sotomayer, W.A. A review of aeroelastic research at the flight dynamics laboratory, Presented at the second international symposium on aeroelasticity and structural dynamics. Aachen, Germany, 1-3 April 1985.Google Scholar
3.22 Coupry, G. Aeroelasticity today and tomorrow, ICAS-86-0.2. ICAS and AIAA 1986.Google Scholar
3.23 Reichert, G. and Strehlow, H. Survey of active and passive means to reduce rotorcraft vibrations. International symposium on aeroelasticity, Nurnberg, Germany, 5-7 October 1981.Google Scholar

7.4 Aeroelasticity papers reviewing research activities at key establishments

4.1 Reed, W.H. Aeroelasticity matters: Some reflections on two decades of testing in the NASA Langley transonic dynamics tunnel, International symposium on aeroelasticity, Nuremberg, Germany, 5-7 October 1981.Google Scholar
4.2 Honlinger, H. and Steininger, M. Survey of aeroelastic wind tunnel and flight testing methods, International symposium on aeroelasticity, Nurnberg, Germany, 5-7 October 1981.Google Scholar
4.3 Potter, D.K. Flight flutter and vibration testing, CI6/76, Presented at symposium on The Interpretation of complex signals from mechanical systems, IMechE 1976, pp 9-16.Google Scholar
4.4 ANON Report on Italian activities in Aeroelasticity, Presented at the 53rd AGARD Structures and Materials Panel — Noordwijkerhout, The Netherlands. Fall 1981.Google Scholar
4.5 Destuynder, R. Recent developments in wing with stores flutter suppression, International symposium on aeroelasticity, Nurnberg, Germany, 5-7 October 1981.Google Scholar
4.6 Sensburg, O. Thirty years of structural dynamic investigations at MBB-UF, MBB publication, S-PUB-399, May 1990.Google Scholar

7.5 Smart structures

5.1 Breitbach, E.J., Lammering, R., Melcher, J. and Nitzche, F. Smart structures research in aerospace engineering, Second European conference on smart structures and materials, Glasgow 1994, pp 11–18.Google Scholar
5.2 Dean, P.D. Intelligent aircraft structures — A technique to verify sensor integrity, Second European conference on Smart Structures and Materials, Glasgow, 1994, pp 59–62 Google Scholar
5.3 Janker, P. and Martin, W. Research need for piezoactuators in adaptive structures. Second European conference on smart structures and materials, Glasgow, 1994, pp 80–85 Google Scholar
5.4 Roberts, S.S.S., Butler, R.J. and Davidson, R. Progress towards a robust, user-friendly, system for active structural damping, Second European conference on smart structures and materials, Glasgow, 1994, pp 117–120.Google Scholar
5.5 Allaei, D. Smart aircraft by continuous condition monitoring of aircraft structures and components, Second European conference on smart structures and materials, Glasgow, 1994, pp 152-155.Google Scholar
5.6 Mukai, Y., Tachibana, E. and Inoue, Y. Active response control using rotor fin for wing-induced structural vibrations, Second European conference on smart structures and materials, Glasgow, 1994, pp 190-193.Google Scholar
5.7 Allaei, D. Vibration and noise control in civil structures by ‘smart' design, Second European conference on smart structures and materials, Glasgow, 1994, pp 198-201.Google Scholar
5.8 Wu, W.B. Dynamic analysis on smart materials, Second European conference on smart structures and materials, Glasgow, 1994, pp 269-272.Google Scholar
5.9 Giurgiutiu, V., Chaudhr, Y.Z. and Rogers, C.A. Efficient use of induced strain actuators in aeroelastic active control, Second European conference on smart structures and materials, Glasgow, 1994, pp 273-276Google Scholar
5.10 Abdul-Wahed, M.N. and Weisshaar, T.A. Finite element modeling of three-dimensional integral sensors for the control of aeroelastic structures, Second European conference on smart structures and materials, Glasgow, 1994. pp 346-349.Google Scholar

7.6 Divergence

6.1 Librescu, L., Meirovitch, L. and Song, O. A refined structural model of composite aircraft wings for the enhancement of vibrational and aeroelastic response characteristics, AIAA-93-1536-CP, 1993.Google Scholar
6.2 Ricketts, R.H. and Doggett, R.V. Wind-tunnel experiments on divergence of forward swept wings, NASA Technical Paper 1685, 1980.Google Scholar
6.3 Blair, M. and Weisshaar, T.A. Swept composite wing aeroelastic divergence experiments, J Aircr, AIAA 81-1670R, November 1982, 19, (11), pp 1019–1024.Google Scholar
6.4 Blair, M. and Weisshaar, T.A. Divergence of swept wings with composite structures, AIAA Aircraft Systems and Technology Conference, AIAA 81-1670, 11-13 August 1981, Dayton, Ohio, USA.Google Scholar
6.5 Griffin, K.E. and Eastep, F.E. Active control of forward-swept wings with divergence and flutter aeroelastic instabilities, J Aircr, October 1982,19, (10), pp 885–891.Google Scholar
6.6 Blair, M. and Weisshaar, T.A. Swept composite wing aeroelastic divergence experiments, J Aircr, November 1982, 19, (11), pp 1019–1024.Google Scholar
6.7 Chipman, R.R, Zislin, A.M. and Waters, C. Control of aeroelastic divergence, J Aircr, December 1983, 20, (12), pp 1007–1013.Google Scholar

7.7 Flutter

7.1 Sensburg, O., Lotze, A. and Haidl, G. Wings with stores flutter on variable sweep wing aircraft, Presented at the 39th Structures and Materials Panel of AGARD in Munich, Germany, 6-12 October 1974.Google Scholar
7.2 Simpson, A. The solution of large flutter problems on small computers, Aeronaut J, April 1984, 88, (874), pp 128–140.Google Scholar
7.3 Lotze, A. Asymmetric store flutter, Presented at the 46th Structures and Materials Panel of AGARD in Aalborg, Denmark, 10-14 April 1978.Google Scholar
7.4 Lotze, A., Sensburg, O. and Kuhn, M. Flutter investigations on a combat aircraft with a command and stability augmentation system, Presented at the AIAA Aircraft Systems and Technology meeting at Los Angeles, California, USA, 4-6 August 1975.Google Scholar
7.5 Baneriee, J.R. Flutter characteristics of high aspect ratio tailless aircraft, J Aircr, September 1984,21, (9), pp 733–736.Google Scholar
7.6 Haidl, G. Active flutter suppression on wings with external stores, Presented at the 37th AGARD Structures and Materials Panel — Den Haag, The Netherlands, 7-12 October 1973.Google Scholar
7.7 Mukhopadhyay, V. Interactive flutter analysis and parametric study for conceptual wing design, AIAA 95-3943, 1st AIAA Aircraft Engineering, Technology and Operations Congress, 19-21 September 1995, Los Angeles, California, USA.Google Scholar
7.8 Ramsay, R.B. Flutter certification and qualification of combat aircraft, British Aerospace Defence (Military Aircraft Division), Warton Aerodrome, Preston, Lancashire, UK.Google Scholar
7.9 Lee, H.P. Divergence and flutter of a cantilever rod with an inter mediate spring support, Int J Solids and Structures, 1995, 32, (10), pp 137–1382.Google Scholar
7.10 Torii, H. and Matsuzaki, Y. Subcritical flutter characteristics of a swept-back wing in a supersonic flow, Transac Japan Soc Aeronaut Space Sciences, August 1995, 38, (120), pp 93–101.Google Scholar
7.11 Mukhopadhay, V. Interactive flutter analysis and parametric study for conceptual wing design, AIAA-95-3943, 1st AIAA Aircraft Engineering, Technology and Operations Congress, 19-21 September 1995, Los Angeles, California, USA.Google Scholar
7.12 ANON A flutter design parameter to supplement the Regier number, AIAA J, July 1964,2, (7), pp 1343–1345.Google Scholar
7.13 Baldelli, D.H., Ohta, H., Matsushita, H., Hashidate, M. and Saitoh, K. Flutter margin augmentation synthesis using normalized coprime factors approach, J Guidance, Control and Dynamics, July-August 1995,18, (4), pp 802–811.Google Scholar
7.14 Karpel, M. Design for active flutter suppression and gust alleviation using state-space aeroelastic modeling, J Aircr, March 1982, 19, (3), pp 221–227.Google Scholar
7.15 Hollowell, S.J. and Dugundii, J. Aeroelastic flutter and divergence of stiffness coupled graphite/epoxy, cantilevered plates. Proceedings 23rd AIAA/ASME/ASCE/AHS Structures and structural dynamics and materials conference, New Orleans, USA, 1982, pp 416-426.Google Scholar
7.16 Hollowell, S.J. and Dugundji, J. Aeroelastic flutter and divergence of stiffness coupled graphite/epoxy cantilevered plates, J Aircr, January 1984,21, (1), pp 69–76.Google Scholar
7.17 Horikawa, H. and Dowell, E.H. An elementary explanation of the flutter mechanism with active feedback controls, J Aircr, April 1979.16,(4), pp 225–232.Google Scholar
7.18 Lottati, I. Flutter and divergence aeroelastic characteristics for composite forward swept cantilevered wing, J Aircr, November 1985,22, (11), pp 1001–1007.Google Scholar
7.19 Baird, E.F. and Clark, W.B. Recent observations on external store flutter, AGARD CP 162, Paper 8, October 1974.Google Scholar
7.20 Chesta, L.A. Parametric study of wing-store flutter, AGARD CP 162, Paper 7, October 1974.Google Scholar

7.8 Aeroservoelasticity

8.1 Noll, T.E. Aeroservoelasticity, Flight-Vehicle Materials, Structures and Dynamics — Assessment and Future Direction, Vol 5 Structural Dynamics and Aeroelasticity, New York, USA, ASME, 1993, Ch 3, pp 179–212.Google Scholar
8.2 Noll, T.E, Blair, M. and Adam, J.C. An aeroservoelastic analysis method for analog or digital systems, J Aircr, November 1986, 23, (11), pp 852–858.Google Scholar
8.3 Cutchins, M.A., Purvis, J.W and Bunton, R.W. Aeroservoelasticity in the time domain, J Aircr, September 1983, 20, (9), pp 753–761.Google Scholar
8.4 Livne, E. and Li, W.-L. Aeroservoelastic aspects of wing/control surface planform shape optimization, AIAA J, February 1995, 33, (2), pp 302–311.Google Scholar
8.5 Caldwell, B.D. and Felton, R. Validation of FCS structural coupling stability characteristics through in-flight excitation, CAES and AIAA International forum on Aeroelasticity and Structural Dynamics, 17-20 June 1997, Rome, Italy.Google Scholar
8.6 Caldwell, B.D. FCS design for structural coupling stability, Aeronaut J, December 1996, 100, (1000), pp 507–519.Google Scholar
8.7 Caldwell, B.D. The FCS/Structural coupling problem and its solution. AGARD CP 560 Paper 16, May 1994.Google Scholar

7.9 Rotary wing aeroelasticity

9.1 Huber, H. and Mikulla, V. Transonic effects on helicopter rotor blades. International symposium on aeroelasticity at Nurnberg, Germany, 5-7 October 1981.Google Scholar
9.2 Ormiston, R.A. and Hodges, D.H. Linear flap-lag dynamics of hingeless helicopter rotor blades in hover, J Amer Heli Soc, April 1972,17,(2), pp 2–14.Google Scholar
9.3 Nagy, E.J. Improved methods in ground vibration testing, J Amer Heli Soc, April 1983, 28, (2), pp 24–29.Google Scholar
9.4 Miller, R.H. and Ellis, C.W. Helicopter blade vibration and flutter, J Amer Heli Soc, July 1956, 1, (3), pp 19–38.Google Scholar
9.5 Lytwyn, R.T., Miao, W. and Woitsch, W. Airborne and ground resonance of hingeless rotors, J Amer Heli Soc, April 1971, 16, (2), pp2–9.Google Scholar
9.6 Loewy, R.G. Helicopter vibrations: a technological perspective, J Amer Heli Soc, October 1984, 29, (4), pp 4–30.Google Scholar
9.7 Loewy, R.G. A two dimensional approximation to the unsteady aerodynamics of rotary wings, J Aeronaut Sci, February 1957, 24, (2), pp 81–92.Google Scholar
9.8 Reed, W.H. Propeller-rotor whirl flutter: A state-of the art review, J Sound and Vibration, 1966, 4, (3), pp 526–544.Google Scholar

7.10 Aeroelastic tailoring

10.1 Shirk, M.H., Hertz, T.J. and Weisshaar, T.A. Aeroelastic tailoring — theory, practice and promise, J Aircr, January 1986, 23, (1), pp 6–18.Google Scholar
10.2 Chuanqi, H. and Xin, Q. Aeroelastic tailoring of aeronautical composite wing structures, Chinese J Aeronaut, May 1991, 4, (2).Google Scholar
10.3 Librescu, L. and Song, O. Static aeroelastic tailoring of composite aircraft swept wings modeled as thin walled beam structures, Achievement in Composites in ‘Japan and the United States, 1990.Google Scholar
10.4 Sherrer, V.C., Hertz, T.J. and Shirk, M.H. Wind tunnel demonstration of aeroelastic tailoring applied to forward swept wings, J Aircr, AIAA, November 1981, 8, (11), pp 976–983.Google Scholar
10.5 Sherrer, V.C., Hertz, T.J. and Shirk, M.H. A wind tunnel demonstration of the principle of aeroelastic tailoring applied to forward swept wings, AIAA 80-0796.Google Scholar
10.6 Lazarus, K.B., Crawley, E.F. and Lin, C.Y. Fundamental mechanisms of aeroelastic control with control surface and strain actuation, J Guidance, Control and Dynamics, January-February 1995,18.Google Scholar
10.7 Yu, J.Y., Kang, W.Y. and Kim, S.J. Elastic tailoring of laminated composite plates by anisotropic piezoelectric polymers — Theory, Computation and Experiment, J Comp Materials, 1995, 29, (9).Google Scholar
10.8 Weisshaar, T.A. Divergence of forward swept composite wings, J Aircr, June 1980,17, (6), pp 442–448.Google Scholar
10.9 Weisshaar, T.A. Aeroelastic tailoring of forward swept composite wings, AIAA 80-0795.Google Scholar
10.10 Weisshaar, T.A. Dynamic stability of flexible forward swept wing aircraft, J Aircr, December 1983, 20, (12), pp 1014–1020.Google Scholar
10.11 Weisshaar, T.A. Experiments on the Divergence of swept wings with composite structures, AIAA Aircraft systems and Technology conference, AIAA-81-1670, 11-13 August 1981, Dayton, Ohio, USA,Google Scholar
10.12 Blair, M. and Weisshaar, T.A. Swept composite wing aeroelastic divergence experiments, J Aircr, November 1982, 19, (11), pp 1019–1024.Google Scholar
10.13 Weisshaar, T.A. Aeroelastic tailoring — creative uses of unusual materials, AIAA 28th structures, structural dynamics and materials conference, AIAA paper 87-0976-CP, 6-8 April 1987, Monterey, California, USA.Google Scholar
10.14 Austin, F., Hadcock, R., Hutchings, D., Sharp, D., Tang, S. and Waters, C. Aeroelastic tailoring of advanced composite lifting surfaces, AIAA 17th structures, structural dynamics and materials conference proceedings, 1976, pp 69-79.Google Scholar