MSC.Nastran Bibliography

Aircraft/Aerospace: Aircraft Design

Abla, Mike H.; Boroughs, Robert R.; Cook, Everett L. Analysis of the Learjet 35/36 Wing and Correlation with Experimental Results, NASTRAN: Users' Exper., pp. 331-352, October, 1976, (NASA TM X-3428). 

Arakaki, Francisco K.; Honda, Filipe K.; Salomão, Maria Luci P. EMB-145 Nose Landing Gear Door Stress Analysis, MSC 1996 World Users' Conf. Proc., Vol. V, Paper No. 45, June, 1996. 

Arnold, Rocky Richard; Collins, Patrick, S. Prediction of Break-Out Patterns for Aircraft Canopies Fragilized Mechanically or with Detonating Cord, MSC 1996 World Users' Conf. Proc., Vol. II, Paper No. 11, June, 1996. 

Bella, David; Hartmueller, Hans; Muehlenfeld, Karsten; Tokar, Gabriel. Identification of Critical Speeds of Rotors Attached to Flexible Supports, The MSC 1993 World Users' Conf. Proc., Paper No. 34, May, 1993. 

Bellenda, R.; Miranda, D.; Pizzamiglio, M. GP-180 Aircraft: F.E.M. Design and Data Management, Proc. of the MSC/NASTRAN Eur. Users' Conf., April, 1985. Paper no. 19. 

Bennett, Robert D. NASTRAN Differential Stiffness Analysis of an Aircraft Canopy, NASTRAN: Users' Exper., pp. 85-106, September, 1971, (NASA TM X-2378). 

Bhatia, Kumar G.; Nagaraja, K. S. Transonic and Density Effect Investigations, Flutter Parametric Studies of Cantilevered Twin-Engine-Transport Type Wing with and without Winglet, Vol. II, September, 1984, (NASA CR-172410). 

Blackburn, Charles L.; Wilhelm, Carl A. NASTRAN Users' Experience of AVCO Aerostructures Division, NASTRAN: Users' Exper., pp. 595-610, September, 1973, (NASA TM X-2893). 

Boroughs, Robert R.; Padmanabhan, Viswa. Determination of Elevator and Rudder Hinge Forces on the Learjet Model 55 Aircraft, Eleventh NASTRAN Users' Colloq., pp. 226-248, May, 1983. 

Boroughs, Robert R. Learjet Model 55 Wing Analysis with Landing Loads, Thirteenth NASTRAN Users' Colloq., pp. 320-340, May, 1985, (NASA CP-2373). 

Bosco, Tran. Geometric Nonlinear Structural Analysis of the Practice Bomb Dispenser Using MSC/NASTRAN, The First Australasian MSC Users Conf. Proc., Paper No. 12, June, 1987. 

Briggs, Hugh C.; Chrisinger, Lance E. A New Capability for Elastic Aircraft Airloads via NASTRAN, Tenth NASTRAN Users' Colloq., pp. 165-186, May, 1982, (NASA CP-2249). 

Carlson, David L.; Shipley, S. A.; Yantis, T. F. Procedure for FRF Model Tuning in MSC/NASTRAN, The MSC 1993 World Users' Conf. Proc., Paper No. 71, May, 1993. 

Chow, E. NASTRAN Nonlinear Analysis of Stiffened Wing Panels, The MSC 1987 World Users Conf. Proc., Vol. I, Paper No. 23, March, 1987. 

Ciuti, Gianluca. Avionic Equipment Dynamic Analysis, MSC 1995 European Users' Conf. Proc., Italian Session, September, 1995. 

Coates, Dr. Tim. Static Analysis of the Wamira Aircraft Using External Superelements, The First Australasian MSC Users Conf. Proc., Paper No. 13, June, 1987. 

Coles, W. A. Structural Computing at the Warton Division of BAE, Proc. of the MSC/NASTRAN Eur. Users' Conf., June, 1983. 

Collier, Craig S.; Spoth, Kevin; Grassi, Glenn. Thermomechanical Finite Element Analysis of Stiffened, Unsymmetric Composite Panels with Two Dimensional Models, The MSC 1993 World Users' Conf. Proc., Paper No. 31, May, 1993. 

Cooper, Michael. The Use of NASTRAN in the Design of Wind Tunnel Research Aircraft, Fifteenth NASTRAN Users' Colloq., pp. 166-183, August, 1987, (NASA CP-2481). 

D'Alessandro Caprice, Manfredo. Finite Element Analysis of Delamination Growth in Compressively Loaded Composite Materials, MSC 23rd European Users' Conf. Proc., Italian Session, September, 1996. 

Darkis, M. Analysis of an Aircraft Engine Mounting Making Use of the Superelement and Material Non-linearity Capability in MSC/NASTRAN, The MSC 1988 World Users Conf. Proc., Vol. II, Paper No. 55, March, 1988. 

de Toledo Fontana, Fabio. Stress Concentration on a Loaded Hole in a Plate in Tension, Proc. of the 2nd MSC/NASTRAN Users' Conf. in Brazil, Paper No. 11, March, 1993, in Portuguese. 

Desy, Philippe; Perron, Claude. Loads Balancing Technique Using MSC/NASTRAN Results, The MSC 1991 World Users' Conf. Proc., Vol. I, Paper No. 16, March, 1991. 

Elchuri, V.; Pamidi, P. R. Dynamic and Aeroelastic Analyses of Turbosystems in NASTRAN, Fourteenth NASTRAN Users' Colloq., pp. 56-59, May, 1986, (NASA CP-2419). 

Frick, Raymond N. Determining Tube Stress From CBEND Element Forces and Moments, The MSC 1993 World Users' Conf. Proc., Paper No. 64, May, 1993. 

Frick, Raymond N. Phd., P.E. Getting FEA Into the Design Process: Rapid Analysis of Tubes, MSC 1995 World Users' Conf. Proc., Paper No. 4, May, 1995. 

Funatogawa, O. Carcass Deflection Analysis of a Turbofan Engine, MSC/NASTRAN Users' Conf. Proc., Paper No. 20, March, 1983. 

Giordano, F.; Santoro, D.; Calcagni, M. Post-Buckling Analysis of the C/E Stiffened Panel of the ATR 42/72 Vertical Fin, MSC 23rd European Users' Conf. Proc., Italian Session, September, 1996. 

Goldberg, Robert K.; Comiskey, Michele D. COMGEN-BEM: Boundary Element Model Generation for Composite Materials Micromechanical Analysis, MSC 1995 World Users' Conf. Proc., Paper No. 23, May, 1995. 

Grosveld, F. W.; Coats, T. J.; Lester, H. C.; Silcox, R. J. Numerical Study of Active Structural Acoustic Control in a Stiffened Double Wall Cylinder, Proceedings of the 1994 National Conference on Noise Control Engineering, Florida, 1994. 

Haggenmacher, Gernot W. The Use of NASTRAN in the Analysis of Large Complex Airframe Structures-Modeling Techniques and Organization, NASTRAN: Users' Exper., pp. 493-516, September, 1971, (NASA TM X-2378). 

Hardman, E. S. Static and Normal Modes Analysis of an Aircraft Structure Using the NASTRAN External Superelement Method, Proc. of the MSC/NASTRAN Eur. Users' Conf., May, 1986. Paper No. 7.

Heerschap M. E. An Interactive Computer Aided Design System for Cut-Outs in Pressurized Aircraft Fuselages, MSC 1995 World Users' Conf. Proc., Paper No. 43, May, 1995. 

Hsu, Lu-Jiin; Chiou, Hua-Tzong; Chen, Kuo-Her. A Study of the Deformation Behavior of Wing for Composite Material, The 2nd Annual MSC Taiwan Users Conf., Paper No. 4, October, 1990. 

Huang, S. L.; Rubin, H. Static and Dynamic Analysis, F-14A Boron Horizontal Stabilizer, NASTRAN: Users' Exper., pp. 251-264, September, 1971, (NASA TM X-2378). 

Jay, Andrew; Lewis, Bryan; Stakolich, Ed. Effect of Time Dependent Flight Loads on Turbofan Engine Performance Deterioration, ASME J. of Engineering for Power, Vol. 104, No. 3, July, 1982. 

Ju, Yeuan Jyh; Ting, Tienko. Modelling and Analysis of an Accelerometer Using MSC/ARIES and MSC/NASTRAN, MSC 1995 World Users' Conf. Proc., Paper No. 22, May, 1995. 

Kamil, S.; Pramono, A.; Santoso, T.; Imadi, A. Stress Analysis of CN-235 FLAPTRACK for Fatigue Life Determination, The MSC 1988 World Users Conf. Proc., Vol. I, Paper No. 33, March, 1988. 

Kamil, Dr. Slulaeman. Some Aspects in Modeling Aircraft Structures, The First Australasian MSC Users Conf. Proc., Paper No. 5, June, 1987. 

Kurokawa, Kunihiko. Superelement Static Analysis for Jet Propulsion Engine Structure, The First MSC/NASTRAN User's Conf. in Japan, October, 1983, in Japanese. 

Lambert, John C. Non-Linear Analysis of a Propeller Blade Retention System, The MSC 1993 World Users' Conf. Proc., Paper No. 32, May, 1993. 

Larkin, Paul A.; Miller, Michael W. STS Coupled Loads Analysis Using MSC/NASTRAN, MSC/NASTRAN Users' Conf. Proc., Paper No. 18, March, 1985. 

Latif, R. Structural Optimization and Its Application to the Design of a CFC Fuselage Structure, The MSC 1988 World Users Conf. Proc., Vol. II, Paper No. 61, March, 1988. 

Lawrence, Charles; Kielb, Robert E. Nonlinear Displacement Analysis of Advanced Propeller Structures Using NASTRAN, National Aeronautics and Space Administration, August, 1984, (NASA TM-83737). 

Lee, Kuan S.; Miller, R. P.; Porada, T. W. An Application of MSC/NASTRAN Transfer Functions for Launch Vehicle Air-Loads Analysis, The MSC 1991 World Users' Conf. Proc., Vol. I, Paper No. 15, March, 1991. 

Lenselink, H. Aerodynamic Loading on a Thrust-Reverser, The MSC 1991 World Users' Conf. Proc., Vol. I, Paper No. 17, March, 1991. 

Lopez, F. de Nicolas; Garcia, M. Huertas. Prediction of Interlaminar Stresses in Skin-Stiffener Interface with MSC/NASTRAN, Proc. of the 19th MSC European Users' Conf., Paper No. 27, September, 1992. 

Marulo, Francesco; Beyer, Todd B. NASTRAN Application for the Prediction of Aircraft Interior Noise, Fifteenth NASTRAN Users' Colloq., pp. 266-285, August, 1987, (NASA CP-2481). 

Mattana, G.; Miranda, D. MSC/NASTRAN Applications in P-180 Analysis, Proc. of the MSC/NASTRAN First Italian Users' Conf., October, 1987. 

Mazet, G. B.; Gillot, E. Static Analysis Using Super-Elements of a Part of an Aircraft Brake Assembly, Proc. of the 17th MSC Eur. Users' Conf., Paper No. 25, September, 1990. 

McClellan, Gisela W. The Structural Finite Element Model of the C-5A, Thirteenth NASTRAN Users' Colloq., pp. 364-376, May, 1985, (NASA CP-2373). 

McLaughlin, A. Finite Element Dynamic Analysis of Production Aircraft, 4th Eur. Rotorcraft and Powered Lift Aircraft Forum, Assoc. Ital di Aeronaut ed Astronaut, pp. 20.1-20.7, September, 1978. 

Melis, Matthew E.; Ogonek, Joseph A. A Life Prediction Algorithm Implemented in P3 Using PCL, MSC 1995 World Users' Conf. Proc., Paper No. 19, May, 1995. 

Mera, A.; Yantis, T. F.; SemGupta, G.; Landmann, A. MSC/NASTRAN Implementation of Coupled Structural-Acoustic Response for Aircraft Cabin Noise Prediction, MSC/NASTRAN Users' Conf. Proc., Paper No. 14, March, 1986. 

Moon, Y. I.; Bharatram, G.; Schimmels, Capt. S. A.; Venkayya, Dr. V. B. A Vulnerability Map of a Commercial Aircraft, MSC 1996 World Users' Conf. Proc., Vol. V, Paper No. 44, June, 1996. 

Moon, Young; Bharatram, Geetha; Schimmels, Capt. Scott; Venkayya, Dr. Vipperla. Vulnerability and Survivability Analysis of Aircraft Fuselage Subjected to Internal Detonations, MSC 1995 World Users' Conf. Proc., Paper No. 11, May, 1995. 

Ouno, Ryuji. Static Analysis for Fan Case of Turbofan Jet Propulsion Engine in Static Equilibrium, The First MSC/NASTRAN User's Conf. in Japan, October, 1983, in Japanese. 

Parnell, L. A. Flutter Analysis of Low Aspect Ratio Wings, Fourteenth NASTRAN Users' Colloq., pp. 247-263, May, 1986, (NASA CP-2419). 

Rienicke, M. J.; Turi, A. S.; Vollan, A. Experience with Aeroelastic Analysis of a Single Engine Turbo Trainer Using Finite Element Methods, Second Int. Symp. on Aeroelasticity and Structural Dynamics-Collected Papers of the Symp., Deutsche Gesellschaft fuer Luft- und Raumfahrt, pp. 286-296, April, 1985. 

Roozen, N. B. Numerical Acousto-Elastic Analysis of Aircraft Structures using MSC/NASTRAN, Proc. of the 20th MSC European Users' Conf., September, 1993. 

Sampica, James D. Finite Element Analysis Applied to Avionics Mount, The 1989 MSC World Users Conf. Proc., Vol. I, Paper No. 19, March, 1989. 

Schips, C. Aero-Engine Turbine Dynamic Analysis, Proc. of the 18th MSC Eur. Users' Conf., Paper No. 8, June, 1991. 

Schwarzmeier, Klaus O. Load Redistribution Method on Aerodynamic Surfaces Using MSC/NASTRAN-A DMAP Application, Proc. of the 2nd MSC/NASTRAN Users' Conf. in Brazil, Paper No. 6, March, 1993, in Portuguese. 

Shah, Lalit C.; Breznak, Ronald. Application of Level 15.9 NASTRAN to a Large Model of B-1 Wing, NASTRAN: Users' Exper., p. 581, October, 1976, (NASA TM X-3428). 

Striz, Alfred G.; Brueckner, Frank P. Finite Element Analysis and Redesign of Jet Engine Starter Breech Chamber, ASME Winter Annual Mtg., December, 1986, (86-WA/DE-20). 

Subrahmanyam, K. B.; Kaza, K. R. V.; Brown, G. V.; Lawrence, C. Nonlinear Vibration and Stability of Rotating, Pretwisted, Preconed Blades Including Coriolis Effects, J. of Aircraft, Vol. 24, No. 5, pp. 342-352, May, 1987. 

Suwandi, Masduki; Witono, Kurnia. N-250 Windshield Finite Element Model, The MSC 1993 World Users' Conf. Proc., Paper No. 78, May, 1993. 

Van Nimwegen, Robert R. High Pressure Turbine Blade Stress Analysis, NASTRAN: Users' Exper., pp. 477-484, September, 1972, (NASA TM X-2637). 

Vollan, A. Use of MSC/NASTRAN for the Aeroelastic Analysis of the Pilatus PlC-9 Turbo Trainer, Proc. of the MSC/NASTRAN Eur. Users' Conf., May, 1986. 

Volpe, Roberto. Airplane Engine Nacelle - Static Nonlinear Analysis by MSC/NASTRAN-SOL66 to Substantiate the Damage Tolerance Capability, Proc. of the 21st MSC European Users' Conf., Italian Session, September, 1994. 

Wellen, H.; Kathmann, C.; Hertl, K. Structural Optimization of Aircraft Components with STARS and MSC/NASTRAN, Proc. of the MSC/NASTRAN Eur. Users' Conf., May, 1987. 

White, John L.; Beste, David L. NASTRAN Applications to Aircraft Propulsion Systems, NASTRAN: Users' Exper., pp. 91-104, September, 1975, (NASA TM X-3278). 

Wilkinson, Michael T.; Bruce, Arthur C. Structural Analysis of Light Aircraft Using NASTRAN, NASTRAN: Users' Exper., pp. 123-124, September, 1973, (NASA TM X-2893). 

Wu, H. T.; Diep, S. Q.; Gupta, V. K. Nonlinear Static Analysis of McDonnell Douglas MD90 Aircraft Using MSC/NASTRAN Superelement Database, The MSC 1991 World Users' Conf. Proc., Vol. II, Paper No. 38, March, 1991. 

Zimmerman, W. Static Analysis of a Gearbox for Flap Actuating System for Airbus A 330/A 340, Proc. of the Sixteenth MSC Eur. Users' Conf., Paper No. 9, September, 1989.