2005 Technical Papers

 

Alpman, E. and Long, L.N., “Separated Turbulent Flow Simulations Using a Reynolds Stress Model and Unstructured Meshes,” Proceedings of the AIAA Aerospace Sciences Meeting, AIAA Paper No. 2005-1094, Reno, NV, January 10-13, 2005.

Jeram, G.J., Sahani, N.A., Prasad, J.V.R., and Horn, J.F., “Distributing Limit Protection between Autonomous Restraint and Voluntary Tactile Cues,” Proceedings of the AIAA Aerospace Science Meeting, AIAA Paper No. 2005-30, Reno, NV, January 10-13, 2005.

Kim, J.S., Wang, K.W., and Smith, E.C., “High-Authority Piezoelectric Actuation System Synthesis through Mechanical Resonance and Electrical Tailoring,” Journal of Intelligent Material Systems and Structures, Vol. 16, January 2005, pp. 21-31.

Kinzel, M.P., Maughmer, M.D., Lesieutre, G.A., and Duque, E.P.N, “Numerical Investigation of Miniature Trailing-Edge Effectors on Static and Oscillating Airfoils,” Proceedings of the AIAA Aerospace Sciences Meeting, AIAA Paper No. 2005-1039, Reno, NV, January 10-13, 2005.

Lee, D., Sezer-Uzol, N., Horn, J.F., and Long, L.N., “Simulation of Helicopter Shipboard Launch and Recovery with Time-Accurate Airwakes,” AIAA Journal of Aircraft , Vol. 42, No. 2, March-April 2005, pp.448-461.

Lee, D., Sezer-Uzol, N., Horn, J.F., and Long, L.N., “Simulation of Pilot Control Activity During Helicopter Shipboard Operations,” AIAA Journal of Aircraft, Vol. 42, (2), March-April 2005, pp.448-461.

Alpman, E. and Long, L. N., “Unstructured Reynolds Stress Model Solutions for Turbulent Flow around a BELL 214ST Fuselage,” Proceedings of the American Helicopter Society 61st Annual Forum,Grapevine, Vol. 1, pp. 370-383, TX, June 1-3, 2005.

Anusonti-Inthra, P., Sarjeant, R., Frecker, M., and Gandhi, F., “Design of a Conformable Rotor Airfoil Using Distributed Piezoelectric Actuators,” AIAA Journal, Vol. 43, No. 8, August 2005, pp. 1684-1695.

Brentner, K.S., Edwards, B.D., Riley, R., and Schillings, J., “Predicted Noise for a Main Rotor with Modulated Blade Spacing,” Journal of the American Helicopter Society, Vol. 50, No. 1, January 2005, pp. 18-25.

Brentner, K.S., Lopes, L.V., Chen, H.N., and Horn, J.F., “Near Real-Time Simulation of Rotorcraft Acoustics and Flight Dynamics,” Journal of Aircraft, Vol. 42, No. 2, March-April 2005, pp. 347-355.
Chen, H.N., Brentner, K.S., and Shirey, J.S., “An Investigation of Transient Rotor Noise in Maneuvering Flight,” Proceedings of the 11th AIAA/CEAS Aeroacoustics Conference (26th AIAA Aeroacoustics Conference), AIAA Paper No. 2005-2903, Monterey, CA, May 23 – 25, 2005.

Chen, H.N., Brentner, K.S., Ananthan, S., and Gordon Leishman, J., “A Computational Study of Helicopter Rotor Wakes and Noise Generated During Transient Maneuvers,” Proceedings of the American Helicopter Society 61st Forum, Vol. 1, pp. 492-517, Grapevine, TX, June 1-3, 2005.

Bridges, D.O., Horn, J.F., and Ray, A., “Model-Following Control of a Military Helicopter with Damage Mitigation,” Proceedings of the AIAA Guidance, Navigation, and Controls Conference, AIAA Paper No. 2005-6347, San Francisco, CA, August 15-18, 2005.

Chen, J., Lagoa, C.M., Horn, J.F., and Ray, A., “Output Bounded Switching Control for Future Generation Rotorcraft,” Proceedings of the AIAA Guidance, Navigation, and Controls Conference,AIAA Paper No. 2005-6371, San Francisco, CA, August 15-18, 2005.

DeSmidt, H.A., Wang, K.W., Smith, E.C., and Provenza, A., “On the Robust Stability of Segmented Driveshafts with Active Magnetic Bearing Control,” Journal of Vibration and Control, Vol. 11, No. 3, March 2005, pp. 317-329.

Gandhi, F. and Bullough, W., “On the Phenomenological Modelling of Electrorheological and Magnetorheological Fluid Pre-Yield Behavior,” Journal of Intelligent Material Systems and Structures,Vol. 16, No.3, March 2005, pp. 237-248.

Munsky, B., and Gandhi, F., “Analysis of Helicopter Blade-Vortex Interaction Noise with Flight Path or Attitude Modification,” Journal of the American Helicopter Society, Vol. 50, No. 2, April 2005, pp. 123-137.

Palacios, J.L. and Smith, E.C., “Dynamic Analysis and Experimental Testing of Thin-Walled Structures Driven by Shear Tube Actuators,” Proceedings of the 46th AIAA/AHS/ASME/ASCE/ASC Structures, Structural Dynamics and Material Conference, AIAA Paper No. 2005-2112, Austin, TX, April 18-21, 2005.

Nampy, S.N. and Smith, E.C., “Extension-Twist Coupled Tiltrotor Blades Using Flexible Matrix Composites,” Proceedings of the46th AIAA/AHS/ASME/ASCE/ASC Structures, Structural Dynamics and Material Conference, AIAA Paper No. 2005-2182, Austin, TX, April 18-21, 2005.

LeHen, F., Smith, E.C., and Lesieutre, G.A., “Actively-Enhanced Periodically-Layered Mount For Helicopter Gearbox Isolation,” Proceedings of the 46th AIAA/AHS/ASME/ASCE/ASC Structures, Structural Dynamics and Material Conference, AIAA Paper No. 2005-2250, Austin, TX, April 18-21, 2005.

Malovrh, B. and Gandhi, F., “Sensitivity of Helicopter Blade-Vortex-Interaction Noise and Vibration to Interaction Parameters,” Journal of Aircraft, Vol. 42, No. 3, May-June 2005, pp. 685-697.

Maughmer, M.D., Lesieutre, G.A., and Kinzel, M.P., “Miniature Trailing-Edge Effectors for Rotorcraft Performance Enhancement,” Proceedings of the American Helicopter Society 61st Forum, Vol. 2, pp. 1886-1897, Grapevine, TX, June 1-3, 2005.

Mayrides, B., Smith, E.C., and Wang, K.W., “Analysis and Synthesis of Highly Flexible Helicopter Drivelines with Flexible Matrix Composite Shafting,” Proceedings of the American Helicopter Society 61st Forum, Vol. 2, pp. 1582-1595, Grapevine, TX, June 1-3, 2005.

Hines, J.A., Muench, D.S., Keller, J.A., and Garga, A.K., “Effects of Time-Synchronous Averaging Implementations on HUMS Features for UH-60A Planetary Carrier Cracking,” Proceedings of the American Helicopter Society 61st Annual Forum, Vol. 1, pp. 218-227, Grapevine, TX, June 1-3, 2005

Horn, J.F., Bridges, D.O., Wachspress, D.A., and Rani, S.L., “Implementation of a Free-Vortex Wake Model in Real-Time Simulation of Rotorcraft,” Proceedings of the American Helicopter Society 61st Annual Forum, Vol. 2, pp. 2057-2074, Grapevine, TX, June 1-3, 2005.

Nissly, A., Anusonti-Inthra, P., Gandhi, F., and Frecker, M., “Design Optimization of a Controllable Camber Rotor Airfoil,” Proceedings of the American Helicopter Society 61st Forum, Vol. 1, pp. 707-716, Grapevine, TX, June 1-3, 2005.

Kim, J.S., Wang, K.W., and Smith, E.C., “Development of a Resonant Actuation System for Active Flap Rotors,” Proceedings of the American Helicopter Society 61st Forum, Vol. 2, pp. 1627-1637, Grapevine, TX, June 1-3, 2005.

Horn, J.F., Bridges, D.O., Lopes, L.V., and Brentner, K.S., “Development of a Low-Cost Multi-Disciplinary Rotorcraft Simulation Facility.” AIAA Journal of Computing, Information, and Communications, Vol. 2, No. 7, July 2005, pp.267-284.

Horn, J.F., Tolani, D.K., Lagoa, C.M., Wang, Q., and Ray, A., “Reliable Operation of Rotorcraft Using Probabilistic Robust Control.” IFAC Control Engineering Practice, Vol. 12, No. 8, August 2005, pp. 1037-1046.

Hanford, S., Long, L.N., and Horn, J.F., “A Semi-Autonomous Quad-Rotor Micro Air Vehicle,”Presented at the AIAA InfoTech@Aeropace Conference, AIAA Paper No. 2005-7077, Washington DC, September 26-29, 2005.

Kim, J.S., Wang, K.W., and Smith, E.C., “Design and analysis of piezoelectric transducer based resonant actuation systems,” Presented at the 2005 ASME International Mechanical Engineering Congress & Exposition, Orlando, FL, November 6-11, 2005.

Lee, D. and Horn, J.F., “Optimization of a Helicopter Stability Augmentation System for Operation in a Ship Airwake,” Proceedings of the American Helicopter Society 61st Annual Forum, Vol. 2, pp. 1149-1159, Grapevine, TX, June 1-3, 2005.

Long, L.N., Hanford, S.D., Niessner, A.F., Gurney, G.B., and Hansen, R.P., “An Undergraduate Course in Unmanned Air Vehicles,” Presented at the AIAA InfoTech@Aeropace Conference, AIAA Paper No. 2005-6982, Washington DC, September 26-29, 2005.

Long, L.N. and Gupta, A., “Scalable Massively Parallel Artificial Neural Networks,”Presented at the AIAA InfoTech@Aeropace Conference, AIAA Paper No. 2005-7168, Washington DC, September 26-29, 2005.

Miller, J.A., Niessner, Jr., A.F., DeLullo, A.M., Minear, P.D., Long, L.N., “Intelligent Unmanned Air Vehicle Flight Systems,” Presented at the AIAA InfoTech@Aeropace Conference, AIAA Paper No. 2005-7081,Washington DC, September 26-29, 2005.

Hanford, S.D., Long, L.N., and Horn, J.F., “A Small Semi-Autonomous Rotary-Wing Unmanned Air Vehicle,” AIAA Paper No. 2005-7077, AIAA InfoTech@Aerospace Conference, Washington D.C., September, 2005.

Modi, A., Sezer-Uzol, N., Long, L.N., and Plassmann, P.E., “Scalable Computational Steering for Visualization/Control of Large-Scale Fluid Dynamics Simulations,” Journal of Aircraft, Vol. 42, No. 4, July-August 2005, pp. 963-975.

Nampy, S.N., Smith, E.C., Shan, Y., and Bakis, C.E., “Extension-Twist Coupled Tiltrotor Blades Using Flexible Matrix Composites,” Presented at the Structures and Survivability Specialists’ Meeting,Williamsburg, VA, October 25-27, 2005.

Perez, G., Brentner, K.S., Brès ,G.A., and Jones, H.E., “A First Step Toward the Prediction of Rotorcraft Maneuver Noise,” Journal of the American Helicopter Society, Vol. 50, No. 3, July 2005, pp. 230-237.

Petrie, J.S., Lesieutre, G.A., and Smith, E.C., “Design and Model Testing of Helicopter Rotor Blade Lag Fluid Embedded Chordwise Inertial Dampers,” Proceedings of the American Helicopter Society 61st Forum, Vol. 1, pp. 994-1004, Grapevine, TX, June 1-3, 2005.

Ramrakhyani, D., Lesieutre, G.A., Frecker, M. and Bharti, S., “Aircraft Structural Morphing Using Tendon Actuated Compliant Cellular Trusses,” Accepted for publication in Journal of Aircraft, 2005.

Sahani, N. and Horn, J.F., “Adaptive Model Inversion Control of a Helicopter with Structural Load Limiting.” Accepted for publication in AIAA Journal of Guidance, Control, and Dynamics, March 2005.

Sahani, N.A. and Horn, J.F., “Command Limiting for Full-Envelope Guidance and Control of Rotorcraft,” Proceedings of the AIAA Guidance, Navigation, and Controls Conference, AIAA Paper No. 2005-6348, San Francisco, CA, August 15-18, 2005.

Sezer-Uzol, N., Sharma, A. and Long, L.N., “Computational Fluid Dynamics Simulations of Ship Airwakes,” To appear Journal of Aerospace Engineering, 2005.

Shan, Y. and Bakis, C.E., “Internal Heating Behavior of Flexible Matrix Composite Driveshaft,”Proceedings of the American Helicopter Society 61st Forum, Vol. 2, pp. 2184-2191, Grapevine, TX, June 1-3, 2005.

Singh, R., F. Gandhi, E. Hathaway, “Wing-Flaperon and Swashplate Control for Whirl-Flutter Stability Augmentation of a Soft-Inplane Tiltrotor,” Proceedings of the 31st European Rortorcraft Forum, Florence, Italy, Sept. 2005.

Sullivan, B.M., Edwards, B.D., Brentner, K.S., and Booth Jr., E.R., “A Subjective Test of Modulated Blade Spacing for Helicopter Main Rotors,” Journal of the American Helicopter Society, Vol. 50, No. 1, January 2005, pp. 26-32.

Thiel, M., “Active Gurney Flaps for Rotorcraft Applications,” Presented at the Mindbend 2005 Student Conference, University Park, PA, April 2005.

Tolani, D.K., Horn, J.F., Yasar, M., and Ray, A., “Hierarchical Control of Rotorcraft for Enhanced Performance and Structural Durability,” Proceedings of the AIAA Guidance, Navigation, and Controls Conference, AIAA Paper No. 2005-6349, San Francisco, CA, August 15- 18, 2005.

Horn, J.F., Tolani, D.K., Lagoa, C.M., Wang, Q., and Ray, A., “Reliable Operation of Rotorcraft Using Probabilistic Robust Control,” IFAC Control Engineering Practice, Vol. 12, (8), August 2005, pp. 1037-1046

Yang, M.Y., Lesieutre, G.A., Hambric, S.A. and Koopmann, G.H., “Development of a Design Curve For Particle Impact Dampers,” Noise Control Engineering Journal, Vol. 53, No.1, January – February 2005, pp. 5-13.

Lee, D. and Horn, J.F., “Simulation of Pilot Workload for a Helicopter Operating in a Turbulent Ship Airwake,”  Journal of Aerospace Engineering – Proceedings of the Institute of Mechanical Engineers Part G, Special issue on shipborne aviation, Vol. 219, (G5), October 2005, pp. 445-458.