Reports, Papers, Articles, and Presentations:
Anees Ahmad and Lamar Hawkins, “Development of Software to Model AXAF-1 Image Quality,” NASA CR-203978 (1996).
F.A. Akyuz and E. Heer, VISCEL Computer Program User Manual for Analysis of Linear Viscoelastic Structures, vol. 1: Users’ Manual, (Pasadena: NASA Jet Propulsion Laboratory, 1971).
B.O. Almroth and F.A. Brogan, “The STAGS Computer Code,” NASA CR-2950 (1978).
B.O. Almroth and A.M. Holmes, “An experimental study of the strength and stability of thin monocoque shells with reinforced and unreinforced rectangular cutouts,” NASA CR-115267 (1971).
Donald J. Baker, “Response of Damaged and Undamaged Tailored Extension-Shear-Coupled Composite Panels,” Journal of Aircraft, vol. 43, No. 2 (2008), pp. 517–527.
Kay S. Bales, “Structural Mechanics Division Research and Technology Plans for FY 1989 and Accomplishments for FY 1988,” NASA TM-101592 (1989).
Karen F. Bartos and Michael A. Ernst, “Evaluation of MARC for the Analysis of Rotating Composite Blades,” NASA TM-4423 (1993).
James L. Beck, “Probabilistic System Identification in the Time Domain,” in USAF–NASA, USAF/NASA Workshop of Model Determination for Large Space Systems (Pasadena: California Institute of Technology, 1988).
Eric B. Becker and Trent Miller, “Final Report: Development of Non-Linear Finite Element Computer Code,” NASA CR-179965 (1985).
Stanley U. Benscoter and Richard H. MacNeal, “Equivalent Plate Theory for a Straight Multicell Wing,” NACA TN-2786 (1952).
Manoj K. Bhardwaj, “Aeroelastic Analysis of Modern Complex Wings Using ENSAERO and NASTRAN,” Progress Report, Virginia Polytechnic Institute and State University (1995).
K.W. Brown, M.S. Hirschbein, and C.C. Chamis, “Finite Element Engine Blade Structural Optimization,” AIAA Paper 85-0645 (1985).
Gerald V. Brown, Robert E. Kielb, Erwin H. Meyn, Richard E. Morris, and Stephen J. Posta, “Lewis Research Center Spin Rig and Its Use in Vibration Analysis of Rotating Systems,” NASA TP-2304 (1984).
Karen F. Bugos and Michael A. Ernst, “Evaluation of MARC for the Analysis of Rotating Composite Blades,” NASA TM-4423 (1993).
J.J. Burken, G.S. Alag, and G.B. Gilyard, “Aeroelastic Control of Oblique-Wing Aircraft,” NASA TM-86808 (1986).
Joseph M. Carlson, “NASA Technology Transfer: The Computer Software Dissemination Program,” in NASTRAN: Users’ Experiences, Langley Research Center (1971).
C.C. Chamis, “CELFE/NASTRAN code for the analysis of structures subjected to high velocity impact,” NASA TM-79048 (1978).
Computer Software Management and Information Center (COSMIC), A Directory of Computer Programs Available from COSMIC, vol. 1 (Athens, GA: University of Georgia, 1967).
Computer Software Management and Information Center (COSMIC), “COSMIC: 1981 Catalog of Computer Programs,” NASA CR-163916 (1981).
Computer Software Management and Information Center (COSMIC), “Monthly Progress Report,” NASA CR-195809 (1994).
James D. Cronkhite, “The NASA/Industry Design Analysis Methods for Vibration (DAMVIBS) Program—Bell Helicopter Textron Accomplishments,” in Raymond G. Kvaternik, ed., A Government/Industry Summary of the Design Analysis Methods for Vibrations (DAMVIBS) Program, NASA CP-10114 (1993).
Robert E. Curry and Alex G. Sim, “In-Flight Total Forces, Moments, and Static Aeroelastic Characteristics of an Oblique-Wing Research Airplane,” NASA TP-2224 (1984).
L. Dequay, A. Lusk, and S. Nunez, “Integrated flow and structural modeling for rocket engine component test facility propellant systems,” AIAA Paper 91-2402 (1991).
Stephen F. Duffy and John P. Gyekenyesi, “CCARES: A computer algorithm for the reliability analysis of laminated CMC components,” NASA TM-111096 (1993).
A.R. Dusto, et al., A Method for Predicting the Stability Characteristics of an Elastic Airplane, vol. 1: FLEXSTAB Theoretical Description, NASA CR-114712 (1974).
Gary L. Farley and Donald J. Baker, “Graphics and Composite Material Computer Program Enhancements for SPAR,” NASA TM-80209 (1980).
R. Gabel, P. Lang, and D. Reed, “The NASA/Industry Design Analysis Methods for Vibration (DAMVIBS) Program—Boeing Helicopters Airframe Finite Element Modeling,” in Raymond G. Kvaternik, ed., A Government/Industry Summary of the Design Analysis Methods for Vibrations (DAMVIBS) Program, NASA CP-10114 (1993).
L. Bernard Garrett, “Interactive Design and Analysis of Future Large Spacecraft Concepts,” AIAA Paper 81-1177 (1981).
J.P. Giesing, T.P. Kalman, and W.P. Rodden, “Correction Factor Techniques for Improving Aerodynamic Prediction Methods,” NASA CR-144967 (1976).
Glenn B. Gilyard, “The Oblique Wing Research Aircraft: A Test Bed for Unsteady Aerodynamic and Aeroelastic Research,” in NASA Langley Research Center, Transonic Unsteady Aerodynamics and Aeroelasticity, pt. 2, Report N89-19247 (1987).
Cody R. Godines and Randall D. Manteufel, “Probabilistic Analysis and Density Parameter Estimation Within Nessus,” NASA CR-2002-212008 (2002).
J.B. Graham and P.L. Luz, “Preliminary In-Flight Loads Analysis of In-Line Launch Vehicles Using the VLOADS 1.4 Program,” NASA TM-1998-208472 (1998).
K.K. Gupta, “STARS: A General-Purpose Finite Element Computer Program for Analysis of Engineering Structures,” NASA RP-1129 (1984).
K.K. Gupta, M.J. Brenner, and L.S. Volker, “Integrated Aeroservoelastic Analysis Capability With X-29A Analytical Comparisons,” AIAA Paper 87-0907 (1987).
K.K. Gupta, M.J. Brenner, and L.S. Voelker, “Development of an Integrated Aeroservoelastic Analysis Program and Correlation With Test Data,” NASA TP-3120 (1991).
G.P. Guruswamy, “ENSAERO: A multidisciplinary Program for Fluid/Structural Interaction Studies of Aerospace Vehicles,” Computing Systems in Engineering, vol. 1, Nos. 2–4, (1990), pp. 237–256.
D.H. Hodges, A.S. Hopkins, D.L. Kunz, and H.E. Hinnant, “Introduction to GRASP: General Rotorcraft Aeromechanical Stability Program—A Modern Approach to Rotorcraft Modeling,” American Helicopter Society 42nd Annual Forum, Washington, DC, June 1986.
A. Stewart Hopkins and Peter Likins, “Analysis of structures with rotating, flexible substructures,” AIAA Paper 87-0951 (1987).
J.C. Hunsaker and E.B. Wilson, “Report on Behavior of Aeroplanes in Gusts,” NACA TR-1 (1915).
Jerald M. Jenkins and Albert E. Kuhl, “Recent Load Calibrations Experience with the YF-12 Airplane,” in James and Associates, eds., YF-12 Experiments Symposium, vol. 1, NASA CP-2054 (1978).
F. Douglas Johnson and Martin Kokus, “NASA Technology Utilization Program: A Summary of Cost Benefit Studies,” NASA CR-201936 (1977).
F. Douglas Johnson, Emily Miller, Nancy Gunderson, Panayes Gatseos, Charles F. Mourning, Thomas Basinger, and Martin Kokus, “NASA Tech Brief Program: A Cost Benefit Evaluation,” NASA CR-201938 (1977).
Wayne Johnson, “A Comprehensive Analytical Model of Rotorcraft Aerodynamics and Dynamics,” pt. III: “Program Manual,” NASA TM-81184/AVRADCOM TR-80-A-7 (1980).
G.K. Jones and K.J. McEntire, “NPLOT: An Interactive Plotting Program for NASTRAN Finite Element Models,” in NASA, 13th NASTRAN Users’ Colloquium (1985).
Rakesh K. Kapania, Manoj K. Bhardwaj, Eric Reichenbach, and Guru P. Guruswamy, “Aeroelastic analysis of modern complex wings,” AIAA-1996-4011 (1996).
Albert Kaufman, “Simplified Method for Nonlinear Structural Analysis,” NASA TP-2208 (1983).
Michael W. Kehoe, Lisa J. Bjarke, and Edward J. Laurie, “An In-Flight Interaction of the X-29A Canard and Flight Control System,” NASA TM-101718 (1990).
Norman F. Knight, Jr., and Charles C. Rankin, “STAGS Example Problems Manual,” NASA CR-2006-214281 (2006).
W.L. Ko, R.D. Quinn, L. Gong, L.S. Schuster, and D. Gonzales, “Reentry Heat Transfer Analysis of the Space Shuttle Orbiter,” in Howard B. Adelman, ed., NASA Langley Research Center Computational Aspects of Heat Transfer in Structures, NASA CP-2216 (1981), pp. 295–325.
Raymond G. Kvaternik, ed., A Government/Industry Summary of the Design Analysis Methods for Vibrations (DAMVIBS) Program, NASA CP-10114 (1993).
H. Lee and J.B. Mason, “NASTRAN Thermal Analyzer: A General Purpose Finite Element Heat Transfer Computer Program,” in NASA Langley Research Center, 2nd NASTRAN Users’ Colloquium (1972).
Arthur W. Leissa, “The Historical Basis of the Rayleigh and Ritz Methods,” in 7th International Symposium on Vibrations of Continuous Systems, Zakopane, Poland, July 2009.
A.F. Leondis, “Large Advanced Space Systems (LASS) Computer Program,” AIAA Paper 79-0904 (1979).
A.F. Leondis, “Large Advanced Space Systems Computer-Aided Design and Analysis Program,” NASA CR-159191 (1980).
R. Levy and S. Wall, “Savings in NASTRAN Decomposition Time by Sequencing to Reduce Active Columns,” in NASA Langley Research Center, NASTRAN: Users’ Experiences (1971).
D.W. Lips, “Approaches and Possible Improvements in the Area of Multibody Dynamics Modeling,” NASA CR-179227 (1987).
J.B. Mason, “The NASTRAN Hydroelastic Analyzer,” NASA TM-X-65617 (1972).
Shivakumar Mettu, et al, “NASGRO 3.0—A Software for Analyzing Aging Aircraft,” in NASA–FAA–DOD, 2nd Joint NASA/FAA/DoD Conference on Aging Aircraft, pt. 2 (Washington, DC: NASA–FAA–DOD, 1999).
Robert R. Meyer, Jr., and V. Michael DeAngelis, “Flight-Measured Aerodynamic Loads on a 0.92 Aspect Ratio Lifting Surface,” in James and Associates, eds., YF-12 Experiments Symposium, vol. 1, NASA CP-2054 (1978).
Roy G. Miller, “Torsion of Wing Trusses at Diving Speeds,” NACA TR-104 (1921).
R.D. Miller, R.I. Kroll, and R.E. Clemmons, Dynamic Loads Analysis System (DYLOFLEX) Summary, vol. 1: Engineering Formulation, NASA CR-2846-1 (1979).
Richard C. Monaghan, “Description of the HiMAT Tailored Composite Structure and Laboratory Measured Vehicle Shape Under Load,” NASA TM-81354 (1981).
Frank F. Monasa and Joseph M. Roche, “Collapse Analysis of a Waffle Plate Strongback for Space Station Freedom,” NASA TM-105412 (1992).
P.L.N. Murthy and C.C. Chamis, “ICAN: Integrated Composites Analyzer,” 25th Structures, Structural Dynamics and Materials Conference, Palm Springs, CA (1984).
N.N. Nemeth, “CARES: Ceramics Analysis and Reliability Evaluation of Structures,” NASA Lewis Research Center Report LEW-15168 (1994).
F.H. Norton and D.L. Bacon, “The Pressure Distribution Over the Horizontal Tail Surfaces of an Airplane II,” NACA TR-119 (1921).
F.H. Norton and W.G. Brown, “Pressure distribution over the rudder and fin of an airplane in flight,” NACA TR-149 (1923).
Neil Otte, “PATRAN-STAGS Translator (PATSTAGS),” NASA TM-100388 (1990).
Henry Pearson, William McGowan, and James Donegan, “Horizontal Tail Loads in Maneuvering Flight,” NACA TR-1007 (1950).
J.P. Raney, D.J. Weidman, and H.M. Adelman, “NASTRAN: Status, Maintenance, and Future Development,” in First NASTRAN Users’ Colloquium, NASA Langley Research Center (1971).
C.C. Rankin, P. Stehlin, and F.A. Brogan, “Enhancements to the STAGS Computer Code,” NASA CR-4000 (1986).
E.S. Reddy and G.H. Abumeri, “Blade Assessment for Ice Impact (BLASIM), User’s Manual, Version 1.0,” NASA CR-19075 (1993).
J.L. Rogers, Jr., “Programming Structural Synthesis System,” NASA Tech Briefs, vol. 10, No. 2 (May 1986), p. 100.
M.J. Rutkowski, “Aeroelastic Stability Analysis of the AD-1 Manned Oblique-Wing Aircraft,” NASA TM-78439 (1977).
Ashish K. Sareen, Daniel P. Schrage, and T.S. Murthy, “Rotorcraft Airframe Structural Optimization for Combined Vibration and Fatigue Constraints,” 47th American Helicopter Society (AHS) Forum, Phoenix, AZ (1991).
Lawrence S. Schuster, “NASTRAN/FLEXSTAB Procedure for Static Aeroelastic Analysis,” NASA TM-84897 (1984).
Walter J. Sefic and Karl F. Anderson, “NASA High Temperature Loads Calibration Laboratory,” NASA TM-X-1868 (1969).
R.L. Sims, “User’s Manual for FSLIP-3, FLEXSTAB Loads Integration Program,” NASA TM-81364 (1981).
James P. Smith, “BUCKY Instruction Manual Version 3.3,” NASA TM-104793 (1994).
Jaroslaw Sobieszczanski-Sobieski, “An Integrated Computer Procedure for Sizing Composite Airframe Structures,” NASA TP-1300 (1979).
Southwest Research Institute, “NESSUS/NASTRAN Interface,” NASA CR-202778 (1996).
Victor W. Sparrow and Ralph D. Buehrle, “Fuzzy Structures Analysis of Aircraft Panels in NASTRAN,” AIAA Paper 2001-1320 (2001).
F.K. Straub, K.B. Sangha, and B. Panda, “Advance finite element modeling of rotor blade aeroelasticity,” American Helicopter Society Journal, vol. 39, No. 2 (Apr. 1994), pp. 56–68.
Nancy P. Sykes, ed., NASA Workshop on Computational Structural Mechanics, NASA CP-10012 (1989).
R.L. Thompson and R.J. Maffeo, “A Computer Analysis Program for Interfacing Thermal and Structural Codes,” NASA TM-87021 (1985).
Mostafa Toossi, Richard Weisenburger, and Mostafa Hashemi-Kia, “The NASA/Industry Design Analysis Methods for Vibration (DAMVIBS) Program—McDonnell Douglas Helicopter Company Achievements,” in Raymond G. Kvaternik, ed., A Government/Industry Summary of the Design Analysis Methods for Vibrations (DAMVIBS) Program, NASA CP-10114 (1993).
William J. Twomey, “The NASA/Industry Design Analysis Methods for Vibration (DAMVIBS) Program—Sikorsky Aircraft—Advances Toward Interacting with the Airframe Design Process,” in Raymond G. Kvaternik, ed., A Government/Industry Summary of the Design Analysis Methods for Vibrations (DAMVIBS) Program, NASA CP-10114 (1993).
Garret N. Vanderplaats, CONMIN: A FORTRAN Program for Constrained Function Minimization, User’s Manual (Moffett Field, CA: Ames Research Center and U.S. Army Air Mobility R&D Laboratory, 1973).
David F. Voracek and Robert Clarke, “Buffet Induced Structural/Flight Control System Interaction of the X-29A Aircraft,” AIAA Paper 91-1053 (2009).
E.P. Warner, “Static Testing and Proposed Standard Specifications,” NACA TN-6 (1920).
Deene J. Weidman, “NASTRAN Status and Plans,” in 4th NASTRAN Users’ Colloquium, 1975.
Anita S. West, and William F. Hubka “Matrix Methods and Automation in Structural Engineering,” NASA CR-71230 (1966).
A.W. Wilhite and J.J. Rehder, “AVID: A Design System for Technology Studies of Advanced Transportation Concepts,” AIAA Paper 79-0872 (1979).
Eleanor C. Wynne, “Structural Dynamics Division Research and Technology Accomplishments for FY 1990 and Plans for FY 1991,” NASA TM-102770 (1991).
William T. Yeager, Jr., “A Historical Overview of Aeroelasticity Branch and Transonic Dynamics Tunnel Contributions to Rotorcraft Technology and Development,” NASA TM-2001-211054 (2001).
A.F. Zahm and L.H. Crook, “Airplane Stress Analysis,” Report No. 82, Aerodynamical Laboratory, Bureau of Construction and Repair, U.S. Navy (1918).
Books and Monographs:
Paul F. Borchers, James A. Franklin, and Jay W. Fletcher, Flight Research at Ames: Fifty-Seven Years of Development and Validation of Aeronautical Technology, 1940–1997, NASA SP-3300 (Washington, DC: NASA, 1998).
John R. Brauer, What Every Engineer Should Know about Finite Element Analysis (New York: Marcel Dekker, 1993).
Glenn Bugos, Atmosphere of Freedom: Sixty Years at the NASA Ames Research Center, NASA SP-4314 (Washington, DC: NASA, 2000).
Paul E. Ceruzzi, Beyond the Limits: Flight Enters the Computer Age (Cambridge: MIT Press, 1989).
Paul E. Ceruzzi, A History of Modern Computing (Cambridge: MIT Press, 1999).
Edward R. Champion, Jr., and J. Michael Ensminger, Finite Element Analysis with Personal Computers (New York: Marcel Dekker, Inc., 1988).
Andrew J. Dunar and Stephen P. Waring, Power to Explore: A History of the Marshall Space Flight Center, 1960–1990, NASA SP-4313, (Washington, DC: NASA, 1999).
Richard P. Hallion and Michael H. Gorn, On the Frontier: Experimental Flight at NASA Dryden (Washington, DC: Smithsonian Books, 2002).
Caleb W. McCormick, The NASTRAN Users’ Manual, NASA SP-222 (1970).
Peter W. Merlin, Mach 3+: NASA/USAF YF-12 Flight Research, 1969–1979, NASA SP-2001-4525, No. 25 in the Monographs in Aerospace History series (Washington, DC: NASA, 2002).
Victor Paschkis and Frederick Ryder, Direct Analog Computers (New York: John Wiley & Sons, Inc., 1968).
Alvin Renetzky and Barbara Flynn, NASA Factbook, (Orange, NJ: Academia Media, 1971).
Gene L. Waltman, Black Magic and Gremlins: Analog Flight Simulations at NASA’s Flight Research Center, No. 20 in Monographs in Aerospace History, NASA SP-2000-4520 (Washington, DC: NASA, 2000).