MSC.Nastran Bibliography

Helicopters/Rotating Structures

(Korean). Vibration Analysis for Outercase in Drum Washer and Floor, MSC 1994 Korea Users' Conf. Proc., December, 1994, in Korean. 

Barnes, R. A.; Schmid, R.; Adrick, H. C. Rotor Dynamic Analysis with MSC/NASTRAN via the Important Modes Method, The 1989 MSC World Users Conf. Proc., Vol. I, Paper No. 13, March, 1989. 

Bedrossian, Herand; Veikos, Nicholas. Rotor-Disk System Gyroscopic Effect in MSC/NASTRAN Dynamic Solutions, MSC/NASTRAN Users' Conf. Proc., Paper No. 12, March, 1982. 

Bella, David F.; Steinhard, E. Critical Frequency Determination of a Flexible Rotating Structure Attached to a Flexible Support, Proc. of the 18th MSC Eur. Users' Conf., Paper No. 28, June, 1991. 

Bindolino, G.; Lanz, M.; Bassoli, M. Optimal Shape of Composite Flexbeams for Helicopter Rotors, MSC 1995 European Users' Conf. Proc., Italian Session, September, 1995. 

Brunken, John E., Jr.; Vlaminck, Robert R. V-22 MSC/NASTRAN Airframe Vibration Analysis and Correlation, American Helicopter Soc. Dynamics Specialists Mtg., Section 7, Vibrations Session II, November, 1989. 

Cronkhite, J. D. Development, Documentation and Correlation of a NASTRAN Vibration Model of the AH-1G Helicopter Airframe, NASTRAN: Users' Exper., pp. 273-294, October, 1976, (NASA TM X-3428). 

Cronkhite, James D.; Smith, Michael R. Experiences in NASTRAN Airframe Vibration Prediction at Bell Helicopter Textron, American Helicopter Soc. Dynamics Specialists Mtg., Section 6, Vibrations Session I, Paper No. 1, November, 1989. 

Drago, Raymond J.; Margasahayam, Ravi. Stress Analysis of Planet Gears with Integral Bearings; 3-D Finite Element Model Development and Test Validation, The MSC 1987 World Users Conf. Proc., Vol. I, Paper No. 4, March, 1987. 

Drago, Raymond J.; Margasahayam, Ravi N. Resonant Response of Helicopter Gears Using 3-D Finite Element Analysis, The MSC 1988 World Users Conf. Proc., Vol. I, Paper No. 20, March, 1988. 

Drago, Raymond J.; Margasahayam, Ravi N. A Non-Linear Finite Element Approach to Gear Tooth Load Sharing Problem, The 1989 MSC World Users Conf. Proc., Vol. I, Paper No. 16, March, 1989. 

Ferg, D.; Foote, L.; Korkosz, G.; Straub, F.; Toossi, M.; Weisenburger, R. Plan, Execute, and Discuss Vibration Measurements, and Correlations to Evaluate a NASTRAN Finite Element Model of the AH-64 Helicopter Airframe, National Aeronautics and Space Administration, January, 1990, (NASA CR-181973). 

Futterer, Arnold T. A NASTRAN Investigation of Simulated Projectile Damage Effects on a UH-1B Tail Boom Model, Ninth NASTRAN Users' Colloq., pp. 161-172, October, 1980, (NASA CP-2151). 

Halcomb, J. R. Application of Component Modes to the Analysis of a Helicopter, Proc. of the MSC/NASTRAN Users' Conf., March, 1979. 

Hashemi-kia, M.; Toossi, M. Finite Element Model Reduction Application to Parametric Studies and Optimization of Rotorcraft Structures, 46th Annual Forum Proc. of the American Helicopter Soc., Part 1, pp. 139-154, May, 1990. 

Hodges, Robert V.; Nixon, Mark W.; Rehfield, Lawrence W. Comparison of Composite Rotor Blade Models: A Coupled-Beam Analysis and an MSC/NASTRAN Finite-Element Model, National Aeronautics and Space Administration, March, 1987, (NASA TM-89024). 

Howells, R. W.; Sciarra, J. J. Finite Element Analysis Using NASTRAN Applied to Helicopter Transmission Vibration/Noise Reduction, NASTRAN: Users' Exper., pp. 321-340, September, 1975, (NASA TM X-3278). 

Howells, R. W.; Sciarra, J. J.; Ng, G. Shek. Thermal and Structural Analysis of Helicopter Transmission Housings Using NASTRAN, NASTRAN: Users' Exper., pp. 353-380, October, 1976, (NASA TM X-3428). 

Kilroy, Kevin L. Instruments that Overcome the Difficulties in Large Finite Element Analysis Problems, Joint American Helicopter Soc., Nanjing Aeronautical Institute Mtg. on The Theoretical Basis of Helicopter Technology, Paper No. 10, November, 1985. 

Kuo, Peter S. Blade Dynamics Analysis Using NASTRAN, NASTRAN: Users' Exper., pp. 251-268, September, 1973, (NASA TM X-2893). 

Lawrence, Charles; Aiello, Robert A.; Ernst, Michael A.; McGee, Oliver G. A NASTRAN Primer for the Analysis of Rotating Flexible Blades, The MSC 1988 World Users Conf. Proc., Vol. I, Paper No. 32, March, 1988. 

MacNeal, R. H. Structural Dynamics of the Heliogyro, National Aeronautics and Space Administration, May, 1971, (NASA CR-1745). 

MacNeal, R. H. The Dynamics of Rotating Elastic Bodies, The MacNeal-Schwendler Corporation, August, 1973, (MSR-36). 

MacNeal, R. H.; Hedgepeth, J. M. Helicopters for Interplanetary Space Flight, 34th Annual National Forum, American Helicopter Soc., May, 1978. 

Magari, P. J.; Shultz, L. A.; Murthy, V. R. Dynamics of Helicopter Rotor Blades, Computers and Structures, Vol. 29, No. 5, pp. 763-776, 1988. 

Melli, R.; Rispoli, F.; Sciubba, E.; Tavani, F. Structural and Thermal Analysis of Avionic Instruments for an Advanced Concept Helicopter, Proc. of the 15th MSC/NASTRAN Eur. Users' Conf., October, 1988. 

Miranda, I.; Arnait, C. Martinez; Azua, J. Ruiz de. Inclusion of Gyroscopic Effects for the Computation of Critical Speeds of Rotor Systems, Proc. of the 15th MSC/NASTRAN Eur. Users' Conf., Paper No. 8, October, 1988. 

Morton, Mark H.; Kaizoji, Allyne. Effects on Load Distribution in a Helicopter Rotor Support Structure Associated with Various Boundary Configurations, 48th Annual Forum Proc. of the American Helicopter Society, Vol. 1, pp. 629-634, 1992. 

Niering, E. Simulation of Run-Up Procedure with Rotating Structures in Transient Response Calculations, Proc. of the MSC/NASTRAN Eur. Users' Conf., Paper No. 6, May, 1987. 

Nowak, William; James, Courtney. Dynamic Modeling and Analysis of Spinning Polygon Assemblies Using MSC/NASTRAN, The MSC 1993 World Users' Conf. Proc., Paper No. 66, May, 1993. 

Ojalvo, I. U. Extensions of MSC/NASTRAN to Solve Flexible Rotor Problems, MSC/NASTRAN Users' Conf. Proc., Paper No. 13, March, 1982. 

Parker, G. R.; Brown, J. J. Kinetic Energy DMAP for Mode Identification, MSC/NASTRAN Users' Conf. Proc., Paper No. 8, March, 1982. 

Parker, Grant. Gear Analysis Using the MSC/NASTRAN Cyclic Symmetry Approach with Enhanced Graphics, MSC/NASTRAN Users' Conf. Proc., Paper No. 5, March, 1984. 

Patel, Jayant S.; Seltzer, S. M. Complex Eigenvalue Analysis of Rotating Structures, NASTRAN: Users' Exper., pp. 197-234, September, 1972, (NASA TM X-2637). 

Rais-rohani, M. Thin Tailored Composite Wing for Civil Tiltrotor, National Aeronautics and Space Administration, Washington, DC., December, 1994. 

Rose, Ted. Using Optimization in MSC/NASTRAN to Minimize Response to a Rotating Imbalance, MSC 1994 Korea Users' Conf. Proc., December, 1994. 

Rose, Ted. Using Dynamic Optimization to Minimize Driver Response to a Tire Out-of-Balance, MSC 1994 Korea Users' Conf. Proc., December, 1994. 

Rose, Ted L. Using Optimization in MSC/NASTRAN to Minimize Response to a Rotating Imbalance, The Sixth Annual MSC Taiwan Users' Conf. Proc., Paper No. D, November, 1994. 

Rotelli, Richard L., Jr.; Jordan, Apostal. Three-Dimensional Stress Analysis of a Helicopter Main Rotor Hub Using Cyclic Symmetry, MSC/NASTRAN Users' Conf. Proc., Paper No. 22, March, 1983. 

Russo, A.; Mocchetti, R. Dynamic Analysis of Loaded Structures in the Helicopter Field, Proc. of the MSC/NASTRAN Eur. Users' Conf., May, 1984. 

Sainsbury-Carter, J. B.; Conaway, John H. NASTRAN Data Generation of Helicopter Fuselages Using Interactive Graphics, NASTRAN: Users' Exper., pp. 661-678, September, 1973, (NASA TM X-2893). 

Salvestro, Livio; Sirocco, Howden; Currie, Andrew. Cyclic Symmetry Analysis of an Air Blower Fan, Seventh Australasian Users Conf. Proc., Sydney, October, 1993. 

Sauer, G.; Wolf, M. Gyroscopic Effects in the Dynamic Response of Rotating Structures, Proc. of the MSC/NASTRAN Eur. Users' Conf., Paper No. 11, May, 1986. 

Scapinello, F.; Colombo, E. An Approach for Detailed Analysis of Complex Structures Avoiding Complete Models, Proc. of the MSC/NASTRAN Eur. Users' Conf., May, 1987. 

Smith, Michael R.; Rangacharyulu, M.; Wang, Bo P.; Chang, Y. K. Application of Optimization Techniques to Helicopter Structural Dynamics, AIAA/ASME/ASCE/AHS/ASC 32nd Structures, Structural Dynamics, and Materials Conf., Part 1, Paper No. 91-0924, pp. 227-237, April, 1991. 

Sreekanta Murthy, T. Design Sensitivity Analysis of Rotorcraft Airframe Structures for Vibration Reduction, Sensitivity Analysis in Engineering, pp. 299-318, September, 1986, (NASA CP-2457). 

Urban, Michael R.; Dobyns, Alan. MSC/NASTRAN Transient Analysis of Cannon Recoil Loads on Composite Helicopters, The MSC 1991 World Users' Conf. Proc., Vol. I, Paper No. 28, March, 1991. 

Vollan, A. Calculation of Coupled Rotating/Non-Rotating Structures Using NASTRAN, Proc. of the MSC/NASTRAN Eur. Users' Conf., June, 1983. 

Vollan, A. Calculation of Coupled Rotating/Non-Rotating Structures Using NASTRAN, Proc. of the MSC/NASTRAN First Italian Users' Conf., October, 1987. 

Wilson, H. E.; Cronkhite J. D. Static and Dynamic Helicopter Airframe Analysis with NASTRAN, NASTRAN: Users' Exper., pp. 611-620, September, 1973, (NASA TM X-2893). 

Wood, P. Application of the Finite Element Method in the Design Analysis of Helicopter Transmission Systems, Proc. of the 15th MSC/NASTRAN Eur. Users' Conf., October, 1988.