Thermal deicing of polymer composite helicopter blades

Materials Research Society Symposium Proceedings

Volumn 851, Issue , 2005, Pages 563-574

  Dutta, Piyush K ^a   Ryerson, Charles C ^a   Pergantis, Charles ^b  

^a Engineering Research and Development Center   (United States)

^b U S ARMY RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

C-SCAN IMAGES; HELICOPTER BLADES; POLYMER COMPOSITES; THERMAL DEICING;

DYNAMIC LOADS; HELICOPTERS; IMAGE PROCESSING; IMAGING TECHNIQUES; POLYMERS; SCANNING; STRENGTH OF MATERIALS; STRESSES; THERMAL CYCLING; THERMAL EFFECTS; TURBOMACHINE BLADES;

COMPOSITE MATERIALS;

EID: 23844447036     PISSN: 02729172     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. Clayton D. Luce, (2000), Ultrasonic Inspection Honeycomb Panels H-60 Main Rotor Blade, 1 May 2000.
2. Tsai S.W. (1986) Composites Design, Think Composites, Dayton, Ohio. Pp 15.11-15.21.
3. Springer, G.S., (1984), Environmental Effects on Composite Materials, Moisture and Temperature Induced Degradation of Graphite Epoxy Composites, Technomic Publishing Company, Lancaster, PA. pp 6-19.
4. Dutta, P.K. (1996) Low-temperature Freeze-thaw Durability of Thick Composites, Composites, Part B: Engineering, Elsvier Science Ltd. Vol. 27B, No. 3/4, pp 371-379.
5. Ryerson, C., T. Gilligan, and G. Koenig, 1999, "Evaluation of Three Helicopter Preflight Deicing Techniques," AIAA Aerospace Sciences, AIAA-98-0578, 11-14 January, Reno, 9 p.
6. Vinson, J.R., and Sierakowski, R.L., (1986), The Behavior of Structures Composed of Composite Materials, Martinus Nijhoff Publishers, pp 104-117