Recent developments in smart structures with aeronautical applications

Smart Materials and Structures

Volumn 6, Issue 5, 1997, Pages

  Loewy, Robert G ^a  

^a Georgia Institute of Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTICS; ACTUATORS; AERODYNAMICS; AEROSPACE ENGINEERING; AIRCRAFT; BUFFETING; FATIGUE OF MATERIALS; FLUTTER (AERODYNAMICS); INTELLIGENT MATERIALS; PERFORMANCE; PIEZOELECTRIC DEVICES; VIBRATION CONTROL;

AEROELASTIC DIVERGENCE; CONTROL SURFACES; FLIGHT CONTROLS;

INTELLIGENT STRUCTURES;

EID: 0031246157     PISSN: 09641726     EISSN: None     Source Type: Journal    
DOI: 10.1088/0964-1726/6/5/001     Document Type: Review

References (60)

1. Jaeger C A and Rogers C A An overview of smart materials & structures USA Army Workshop
2. Suplee C 1997 Structures with a sense of self Washington Post January 6 p A3
3. Rogers C A 1995 Intelligent materials Sci Am. September 154-7
4. 1993 American Heritage College Dictionary 3rd edn (Houghton Mifflin)
5. Janker P and Martin W 1995 Performance and characteristics of actuator material Proc. 4th Int. Conf. on Adaptive Structures (Cologne) pp 126-38
6. Anderson E H. Moore D M and Fanson J L 1990 Development of an active member using piezoelectric and electrostrictive actuation for control of precision structures Proc. 31st SDM Conf. AIAA (Long Beach) pp 2221-33
7. Mason W P 1935 An electromechanical representation of a piezoelectrical crystal used as a transducer Proc. IRE 1252-63
8. Langevin R A 1954 The electro-acoustic sensitivity of cylindrical ceramic tubes J. Acousi. Soc. Am. 26 421-7
9. Agnes G S and Sendeckyj G P 1993 Smart structures research direction of the USAF Wright Laboratory Structures Division Proc. 4th Int. Conf. on Adaptive Structures (Cologne) pp 3-14
10. Austin F, Knowles G J, Jung W G, Tung C C and Sheedy E M 1992 Adaptive/conformal wing desing for future aircraft Proc. 1st Eur. Conf. on Smart Structures (Glasgow)
11. Austin F, Rossi M J, Jameson A, Van Nostrand W, Su J and Knowles G 1992 Active rib experiment for adaptive conformal wing Proc. 3rd Int. Conf. on Adaptive Structures (San Diego, Ca) pp 43-55
12. Rossi M J, Austin F and Vao Nostrand W 1993 Active rib experiment for shape control of an adaptive wing Proc. 34th SDM Conf. (La Jolla. CA) pp 3485-98
13. Bauchau O, Loewy R and Bryan P 1986 An Approach to ideal twist distribution in tilt rotor VTOL blade designs Rensselaer Rotorcraft Technology Center Report D-86-2
14. Chen P C and Chopra I 1996 Induced strain actuation of composite beams and rotor Induced with embedded piezoceramic elements Smart Mater. Struct. 5 35-48
15. Ho C-M. Tung S and Lee G-B 1997 MEMS - a technology for advancements in aerospace engineering 35th Aerospace Sciences Meeting &. Exhibit (Remo, NV, 1997)
16. Lester H C and Fuller C R 1986 Active control of propeller induced noise fields inside a flexible cylinder AIAA 10th Areoacoustics Conf. (Seattle, WA)
17. Ushijima T and Kumakawa S Active engine mount with piezo-actuator for vibration control Society of Automotive Engineering Paper 930201
18. Ehlers S M and Weishaar T A 1990 Static aeroelastic behavior of an adaptive laminated piexoelectric composite wing 31st SDM Conf. (Long Beach. CA) (AIAA) pp 1611-23
19. Weisshaar T A 1978 Aeroelastic stability and performance characteristics of aircraft with advanced composite swept forward wing structures AFFDL-TR-78-116
20. Ehlers S M and Weisshaar T A 1992 Adaptive wing flexural axis control 3rd Int. Conf. an Adaptive Structures (San Diego, CA) pp 28-40
21. Santini P, Gasbarri P, Altobelli M and Rossi A 1994 A comparative overview of strain actuated surfaces' design 5th Int Conf. on Adaptive Structures (Sondai) pp 21-33
22. Lazarus K B and Crawley E F 1992 Multivariable active lifting surface control using strain actuation: analytical and experimental results 3rd Int. Conf. on Adaptive Structures (San Diego, CA) pp 87-101
23. Friedmann P P 1993 Aeroelastic, aeromechanical and vibration problems in helicopters Proc. 33rd Israel Ann. Conf, on Aviation and Astronautics pp 37-82
24. Shaw J and Albion N 1981 Active control of the helicopter rotor for vibration reduction J. Am. Helicopter Soc. 26 32-9
25. Wood E, Powers R, Cline J and Hammond C 1985 On developing and flight testing a higher harmonic control system J. Am. Helicopter Soc. 30 3-20
26. Ham N, Behal B and McKillip R Jr 1983 Helicopter rotor lag damping augmentation through individual blade control Vertica 7 361-71
27. Ham N D 1985 Helicopter gust alleviation, attitude stabilization and vibration alleviation using individual-blade-control through a conventional swashplate Proc. 11th Eur. Rolorcraft Forum (London) pp 75-1-5
28. Fulton M V and Ormiston R A 1997 Hover testing of a small-scale rotor with on-blade elevons AHS 53rd Annual Forum (Virginia Beach, VA, 1997)
29. Friedmann P P and Millott T A 1994 Vibration reduction in rotorcraft using active control: a comparison of various approaches J. Guidance Control Dynam. 18 664-73
30. Spangler R L Jr and Hall S R 1990 Piezoelectric actuators for helicopter rotor control 31st SDM Conf. Proc. (Long Beach, CA) pp 1589-99
31. Hall S R and Prechtl E F 1996 Development of a piezoelectric servoflap for helicopter rotor control Smart Mater. Struct. 5 26-34
32. Straub F K and King R J 1996 Application of smart materials to control of a helicopter rotor SPIE Symp. on Smart Structures and Materials (San Diego. CA)
33. Straub F K and Hassan A A 1996 Aeromechanic considerations in the design of a rotor with smart material actuated trailing edge flaps Proc. AHS 52nd Annual Forum (Washington, DC) pp 704-14
34. Millott T and Friedmann P 1992 Vibration reduction in helicopter rotors using an active control surface located on the blade 33rd SDM Proc. (Dallas, TX, 1992) pp 1975-88
35. Millott T A and Friedmann P 1993 The practical implementation of an actively controlled flap to reduce vibrations in helicopter rotors Proc. AHS 49th Ann. Forum (Washington, DC, 1979) pp 1079-92
36. Millot T A and Friedmann P 1994 Vibration reduction in hingeless rotors using an actively controlled trailing edge flap: implementation and time domain simulation 35th SDM Proc (Hilton Head, SC, 1994) pp 8-22
37. Millott T A and Fnedmann P 1994 Magnetostrictively actuated control flaps for vibration reduction in helicopter rotors Proc 2nd Int. Conf on Intrlligent Materials (Williamsburg. VA) (Technomic) pp 900-13
38. Friedmann P. Carman G P and Millott T A 1996 Magnetostrictively actuated control flaps for vibration reduction in helicopter rotors - design consideration for implementation Proc 36th Israel Ann. Conf. on Aerospace Sciences pp 295-306
39. Bothwell, Chandra and Chopra I 1994 Torsional actuation with extension torsion composite coupling and a magnetostrictive actuator 35th SDm Conf. and Adaptive Structures Forum Proc (Hilton Head, SC, 1994)
40. Bernhard A P F and Chopra I 1995 Development and hover testing of a smart trailing edge flap with a piezo-induced bending-torsion coupled actuator AHS Natianal Technical Specalists' Meeting on Rotorcraft Structures (Williamsburg, VA. 1995)
41. Bernhard A P F and Chopra I 1996 Development of a smart moving blade tip activated by a piezo-induced bending-torsion coupled beam SPIE Conf. on Smart Structures and Integrated Systems (San Diego. CA. 1996) pp 19-35
42. 1997 Testing of a smart moving blade tip activated via an enhanced piezo-induced bending-torsion coupled beam AHS 53rd. Annual forum (Virginia Beach. VA. 1997)
43. Barren R 1992 Aeroservoelastic DAP missile fin development 3rd Int. Conf. on Adaptive Structures (San Diego. CA. 1992)
44. Straub F K 1996 A feasibility study of using smart materials for rotor control Smart Mater. Struct. 5 1-10
45. Barrett R and Stutts J 1996 The solid stste adaptive rotor design, development and implication for future rotorcraft AGARD Flight Vehicle Integration Panel Symp. on Advances in Rotorcraft Technology (Ottawa, 1996)
46. Barrett R, Frye P and Schliesman M 1996 Design, development and testing of a solid state adaptive rotor SPIE Symp. on Smart Materials, Structures and MEMS, Indian Institute of Science (Bangalore, 1996)
47. Bent A A and Hagood N W 1995 Improved performance in piezoelectric fiber composites using interdigitated electrodes North Am. Conf. on Smart Structures and Materials (San Diego, CA, 1995)
48. Derham R C and Hagood N W 1996 Rotor design using smart materials to actively twist blades AHS 52nd Ann. Forum (Washington, DC, 1996)
49. Rogers J P, Bent A A and Hagood N W 1996 Characterization of interdigitated electrode piezoelectric fiber composites under high electrical and mechanical loading SPIE (San Diego, CA, 1996)
50. Straub F K 1993 A feasibility study of using smart materials for rotor control AHS 49th Ann. Forum (St Louis. MO. 1993)
51. Roglin R L and Hanagud S V 1996 A helicopter with adaptive rotor blades for collective control Smart Mater. Struct. 5 1-10
52. Straub F K and Merkley D J 1995 Design of a smart material actuator for rotor control SPIE North Am. Conf. on Smart Structures and Materials (San Diego. CA. 1995)
53. Kolm H H and Kolm E A 1984 Spiral piezoelectric rotary actuator Patent 4435667
54. Miura K, Sakamaki M, Ono Y and Suzuki K 1992 A new concept of actuator with large displacements 3rd Int. Conf. on Adaptive Structure (San Diego, CA, 1992) pp 43-55
55. French J D, Weitz G E, Luke J E and Cass R B 1996 Production of continuons piezoelectric fibers for sensor/actuator applications Proc. Ann. Meeting Int. Soc. Appl. Ferroelectr. (New Brunswick, NJ, 1996)
56. Timoshenko S 1941 Strength of Materials Part II, Advanced Theory and Problems (New York: Van Nostrand) pp 292-9
57. Loewy R C and Tseng S P 1993 Smart structures stabilized unstable control surfaces 34th SDM conf. (La Jolla, CA, 1993)
58. Loewy R G and Tseng S P 1993 Exploiting instabilities for control purposes using smart structures Advances in Aerospace Sciences Proc. Seminar in Tribute to Prof Holt Ashley (Stanford, CA, 1993) pp 347-55
59. Theodorsen T 1935 General theory of aerodynamic instability and the mechanism of flutter NACA Report 496
60. Loewy R G and Tseng S P 1995 Tests of an unstable lifting surface stabilized by a stmulated smart structure 6th ARO Int. Workshop on Dynamics and Aeroelastic Stability Modeling of Rotorcraft Systems (Los Angeles. CA, 1995)