Performance predictions of a blade twist actuator system

Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting

Volumn 21, Issue , 2007, Pages 14515-14524

  Caldwell, Nicholas ^a,c,d   Gutmark, Ephraim ^a,c,d   Ruggeri, Robert ^b,d  

^a UNIVERSITY OF CINCINNATI   (United States)

^b BOEING COMPANY   (United States)

^c ML0070 ^*

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; HEAT TRANSFER; MASS TRANSFER; MATHEMATICAL MODELS; OPTIMIZATION; THERMOELECTRICITY; TURBOMACHINE BLADES;

OPERATING CONDITIONS; STARTUP CONDITIONS;

ACTUATORS;

EID: 34250812598     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-1216     Document Type: Conference Paper

References (6)

1. Kota, S., Hetrick, J., and Osborn, R., "Adaptive Structures: Moving into the Mainstream", Aerospace America, No. 9, 2006, pp. 16-18.
2. Roglin, R.L., Kondor, S., and Hanagud, S., "Adaptive Airfoils for Helicopters", AIAA/ASME Adaptive Structures Forum, Hilton Head, SC, 21-22 Apr 1994, AIAA 1994-1764.
3. nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Lake Buena Vista, FL, 1996, AIAA 1996-2805.
4. th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Newport, Rhode Island, 2006, AIAA 2006-2142.
5. Caldwell, N., Glaser, A., Gutmark, E. and Ruggeri, R., "Heat Transfer Model for Blade Twist Actuator System," Accepted for publication in the Journal of Thermophysics and Heat Transfer, September 2006.
6. th AIAA Thermophysics Conference, Orlando, FL, 2003, AIAA 2003-4202.