NASA's Contributions to Aeronautics, Volume 1 by National Aeronautics & Space Administration. - HTML preview

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Endnotes

[1]. There are many topics touching on structural analysis and loads prediction, which the author has not covered. Materials science is excluded, for this paper considers methods for predicting the macroscopic characteristics of a structure, not analyzing the microscopic properties of the materials from which it is built. So too are computer-aided design, computational fluid dynamics, multidisciplinary optimization, structural test and data analysis techniques, and nondestructive inspection/evaluation, aside from passing reference. Though this paper focuses on NASA activities and contributions, there is no intent to minimize the importance of contributions from the aircraft industry, the technical software industry, universities, and other research organizations.

[2]. A.F. Zahm and L.H. Crook, “Airplane Stress Analysis,” Report No. 82, Aerodynamical Laboratory, Bureau of Construction and Repair, U.S. Navy (1918); Roy G. Miller, “Torsion of wing trusses at diving speeds,” NACA TR-104, Langley Research Center (1921); F.H. Norton and D.L. Bacon, “The pressure distribution over the horizontal tail surfaces of an airplane II,” NACA TR-119, Langley Research Center (1921); Norton and W.G. Brown, “Pressure distribution over the rudder and fin of an airplane in flight,” NACA TR-149, Langley Research Center (1923); J.C. Hunsaker and E.B. Wilson, “Report on Behavior of Aeroplanes in Gusts,” Massachusetts Institute of Technology (1915), (prepared by MIT and predating the establishment of the NACA but listed and marked as NACA-TR-1); E.P. Warner, “Static Testing and Proposed Standard Specifications,” NACA TN-6, Langley Field, VA (July 1920), p. 1.

[3]. W. Jefferson Stroud, e-mail message to author, Mar. 29, 2009.

[4]. Stroud, e-mail to author.

[5]. Interview of Annie J. Easley by Sandra Johnson, Cleveland, OH, Aug. 21, 2001, pp .2, 8, in NASA Oral History Project, on NASA Glenn Research Center History Office Web site at http://grchistory.grc.nasa.gov/index.cfm, accessed Apr. 29, 2009.

[6]. Henry Pearson, William McGowan, and James Donegan, “Horizontal Tail Loads in Maneuvering Flight,” NACA TR-1007, Langley Aeronautical Laboratory, VA (1950); Interview of Gonzalo Mendoza and Zachary Hazen by author, Wichita, KS, Apr. 6, 2009.

[7]. 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.

[8]. “Carlo Alberto Castigliano,” at http://www-groups.dcs.st-and.ac.uk/~history/Biographies/Castigliano.html, accessed May 22, 2009.

[9]. Stanley U. Benscoter and Richard H. MacNeal, “Equivalent Plate Theory for a Straight Multicell Wing,” NACA TN-2786 (1952), p. 1.

[10]. Benscoter and MacNeal, “Equivalent Plate Theory,” NACA TN-2786, p. 28.

[11]. Victor Paschkis and Frederick Ryder, Direct Analog Computers (New York: John Wiley & Sons, Inc., 1968), preface.

[12]. Paschkis and Ryder, p. 383.

[13]. Glenn Bugos, Atmosphere of Freedom: Sixty Years at the NASA Ames Research Center, NASA SP-4314 (Washington, DC: NASA, 2000), pp. 181–182.

[14]. Gene Waltman, Black Magic and Gremlins, pp. 1–4.

[15]. Jeremy Meyers, “A Brief History of the Computer (b.c. – 1993a.d.),” on Meyers’s Web site at http://www.jeremymeyers.com/comp#EDC, accessed Apr. 29, 2009; see also Paul E. Ceruzzi, A History of Modern Computing (Cambridge: MIT Press, 1999), pp. 7, 15, 20–21.

[16]. Meyers, “A Brief History of the Computer (b.c. – 1993a.d.).”

[17]. M.J. Turner, R.W. Clough, H.C. Martin, and L.J. Topp , “Stiffness and deflection analysis of complex structures,” Journal of the Aeronautical Sciences, vol. 23 (1956), pp. 805–823.

[18]. John R. Brauer, What Every Engineer Should Know about Finite Element Analysis (New York: Marcel Dekker, 1993), pp. 2–3; Edward R. Champion, Jr., and J. Michael Ensminger, Finite Element Analysis with Personal Computers (New York: Marcel Dekker, Inc., 1988), p. 1.

[19]. Thomas J. Butler, “Operating in the Age of NASTRAN ,” p. 1.

[20]. Anita S. West and William F. Hubka, “Matrix Methods and Automation in Structural Engineering,” NASA CR-71230 (1966), p. 12.

[21]. Butler, “Operating in the Age of NASTRAN,” p. 2.

[22]. C. Thomas Modlin, Jr., e-mail message to author, Apr. 23, 2009.

[23]. Caleb W. McCormick, The NASTRAN Users’ Manual, NASA SP-222 (1970), p. i.

[24]. Butler, “Age of NASTRAN,” p. 2.

[25]. “Matrix Methods in Structural Mechanics,” Air Force Flight Dynamics Laboratory, Wright-Patterson Air Force Base, OH, (proceedings published Nov. 1966, conference date unknown); abstract on Defense Technical Information Center Web site at http://oai.dtic.mil/oai/oai?verb=getRecord&metadataPrefix=html&identifier=AD0646300, accessed May 25, 2009.

[26]. Butler, “Age of NASTRAN,” pp. 3–4.

[27]. McCormick, The NASTRAN Users’ Manual, p. iii; Butler, “Age of NASTRAN,” pp. 4–6; Butler also lists many more members and describes their contributions. At time of writing, document is available in the Tenth NASTRAN Users’ Colloquium, NASA CP-2249, on the NASA Technical Reports Server at http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/198.300.04182_198.300.4182.pdf, accessed Aug. 13, 2009.

[28]. 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), p. 1.

[29]. McCormick, NASTRAN User’s Manual, pp. iii–iv.

[30]. Butler, “Age of NASTRAN,” p. 7.

[31]. Ibid., pp. 2–3.

[32]. Raney, Weidman, and Adelman, 1971, in First NASTRAN Users’ Colloquium, p. 1.

[33]. Ibid., p. 2.

[34]. Foreword to the First User’s Colloquium, 1971.

[35]. McCormick, The NASTRAN User’s Manual, pp. vii–viii.

[36]. Raney, Weidman, and Adelman, “NASTRAN: Status, Maintence, and Future Development,” in First NASTRAN Users’ Colloquium, NASA Langley Research Center (1971).

[37]. Ibid.

[38]. 5th NASTRAN Users’ Colloquium, 1976, pp. 331–352; 8th, 1979, pp. 11–32; 9th, 1980, pp. 201–223; 11th, 1983, pp. 226–248; and 13th, 1985, pp. 320–340.

[39]. “Aircraft Design Analysis,” in Spinoff, NASA, 1979, p. 63.

[40]. 15th NASTRAN Users’ Colloquium, 1987, pp. 166–183.

[41]. Rainey and Weidman, “NASTRAN: A Progress Report,” 2nd NASTRAN Users’ Colloquium (1972), p. 1.

[42]. 2nd NASTRAN Users’ Colloquium, p. 421.

[43]. Additional information is provided in the appendixes.

[44]. Harry G. Schaefer, “Implementation of Mixed Formulation Elements in PC/NASTRAN,” in 21st NASTRAN Users’ Colloquium (1992), pp. 1–7.

[45]. J.P. Giesing, T.P. Kalman, and W.P. Rodden, “Correction Factor Techniques for Improving Aerodynamic Prediction Methods,” NASA CR-144967 (1976).

[46]. Interview of Thomas Christy and John Splichal (aircraft industry) by author, Wichita, KS, May 12, 2009.

[47]. “MSC Software Highlights” on MSC Web site at http://www.mscsoftware.com/about/history.cfm?Q=135&Z=339&Y=346, accessed Feb. 12, 2009.

[48]. 14th User Colloquium, 1986, p. 1.

[49]. Butler, “Age of NASTRAN,” p. 7.

[50]. Ibid., p. 8.

[51]. “Stresses and Strains,” Spinoff, 1998.

[52]. Federal Trade Commission news release, “MSC Software Settles FTC Charges by Divesting Nastran [sic] Software,” Aug. 14, 2002, at http://www.ftc.gov/opa/2002/08/mscsoftware.shtm, accessed May 14, 2009.

[53]. John P. Gyekenyesi, “SCARE: A Post-Processor Program to MSC/NASTRAN,” abstract from NASA Technical Reports Server at http://ntrs.nasa.gov; Karen F. Bartos and Michael A. Ernst, “Evaluation of MARC for the Analysis of Rotating Composite Blades,” NASA TM-4423 (1993), p. 1; and Jim Loughlin, “FEM and Multiphysics Applications at NASA/GSFC,” NASA Goddard Space Flight Center, in 2004 ANSYS Conference, May 24, 2004, Greenbelt, MD; view graph presentation on NASA Technical Report Server at http://ntrs.nasa.gov, accessed May 12, 2009.

[54]. F. Douglas Johnson and Martin Kokus, “NASA Technology Utilization Program: A Summary of Cost Benefit Studies,” NASA CR-201936 (1977), pp. i, 3. See also Johnson, Emily Miller, Nancy Gunderson, Panayes Gatseos, Charles F. Mourning, Thomas Basinger, and Kokus, “NASA Tech Brief Program: A Cost Benefit Evaluation,” NASA CR-201938 (1977); and Spinoff, 1991, pp. 132–143.

[55]. Joseph M. Carlson, “NASA Technology Transfer: The Computer Software Dissemination Program,” in NASTRAN: Users’ Experiences, Langley Research Center (1971), pp. 551–552.

[56]. Computer Software Management and Information Center (COSMIC), A Directory of Computer Programs Available from COSMIC, vol. 1, (Athens, GA: University of Georgia, 1967).

[57]. Carlson, “NASA Technology Transfer,” pp. 551–552.

[58]. COSMIC, “COSMIC: 1981 Catalog of Computer Programs,” NASA CR-163916 (1981), abstract, on NASA Technical Reports Server at http://ntrs.nasa.gov, accessed Mar. 16, 2009.

[59]. COSMIC, “Monthly Progress Report,” NASA CR-195809 (1994), pp. 1–3; Innovation, vol. 1, No. 6 (Nov./Dec. 1993), at http://ipp.nasa.gov/innovation/Innovation16/SoftwareWarehouse.html, accessed Feb. 11, 2009.

[60]. COSMIC, A Directory of Computer Programs Available from COSMIC, vol. 1 (Athens, GA: University of Georgia, 1967).

[61]. Johnson and Kokus, “Summary of Cost-Benefit Studies.”

[62]. Open Channel Foundation, “About the Open Channel Foundation and Open Channel Software” at http://www.openchannelfoundation.org, accessed Feb. 10, 2009; “NTTC and Open Channel Software Launch NASA Software Applications Collection as Space Agency Celebrates Birthday,” Oct. 10, 2001; “Open Channel Publishes the NASA COSMIC Collection,” at http://www.openchannelfoundation.org/cosmic, Open Channel Foundation, accessed Feb. 12, 2009. A list of NASA-developed programs for finite element analysis is reported in Appendix D. As of this writing, the programs and related tasks are available through the Open Channel Foundation Web site. All except GEOFEST were originally released through COSMIC.

[63]. Interview of Chittur Venkatasubban by author, Wichita, KS, May 14, 2009.

[64]. Jennifer Ross-Nazzal, e-mail to author, Apr. 10, 2009; NASA, 9th NASTRAN Users’ Colloquium; Two Centers are not discussed in great detail because they undertake little work in computational structural analysis: the Kennedy Space Center and the Stennis Space Center. With responsibility for spacecraft launch operations, vehicle preparation, and integration, Kennedy maintains a minimal structural engineering staff, which is concerned primarily with supporting the Center’s launch equipment. Thus, this Center is not active in structural analysis methods research and development, though it did host the 9th NASTRAN Users’ Colloquium. The primary mission of Stennis is to test a very specific type of hardware, namely the ground-testing of rocket engines. More recently, it has added research in remote sensing. But with the exception of a small number of studies related to the operation of the Center’s own test equipment, the Stennis Space Center’s involvement in research and development in computational methods is minimal. For more information, see John D. Anderson, Jr., “NASA and the Evolution of Computational Fluid Dynamics,” a companion essay in this volume.

[65]. For more information, see Anderson, “NASA and the Evolution of Computational Fluid Dynamics.”

[66]. Interview of John Gallman by author, Wichita, KS, Apr. 4, 2009.

[67]. 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), p. 67.

[68]. Wayne Johnson, “A Comprehensive Analytical Model of Rotorcraft Aerodynamics and Dynamics, Part III: Program Manual,” NASA TM-81184/AVRADCOM TR-80-A-7, Ames Research Center and U.S. Army Aviation Research and Development Command, June 1980, p. vii.

[69]. 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.

[70]. A. Stewart Hopkins and Peter Likins, “Analysis of structures with rotating, flexible substructures,” AIAA Paper 87-0951 (1987); 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,” 42nd American Helicopter Society, Washington, DC (1986).

[71]. 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).

[72]. 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).

[73]. “Aircraft Design Software,” Spinoff, 1997, p. 107; Phoenix Integration, “About Phoenix,” on Phoenix Integration Web site at http://www.phoenix-int.com/about/company_profile.php, accessed May 11, 2009.

[74]. 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.

[75]. Manoj K. Bhardwaj, “Aeroelastic Analysis of Modern Complex Wings Using ENSAERO and NASTRAN,” Progress Report, Virginia Polytechnic Institute and State University (1995); and Rakesh K. Kapania, Bhardwaj, Eric Reichenbach, and Guruswamy, “Aeroelastic Analysis of Modern Complex Wings,” AIAA-96-4011 (1996).

[76]. Author’s experience.

[77]. Richard P. Hallion and Michael H. Gorn, On the Frontier: Experimental Flight at NASA Dryden (Washington, DC: Smithsonian Books, 2002), pp. 344–354.

[78]. Martin Brenner, e-mail message to author, May 8, 2009.

[79]. 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.

[80]. K.K. Gupta, “STARS—A General-Purpose Finite Element Computer Program for Analysis of Engineering Structures,” NASA RP-1129 (1984); Gupta, M.J. Brenner, and L.S. Voelker, “Development of an Integrated Aeroservoelastic Analysis Program and Correlation With Test Data,” NASA TP-3120 (1991); and Brenner, e-mail message to author, May 8, 2009.

[81]. Interview of Charles Blankenship by author, Mar. 26, 2009.

[82]. Search of NASA Technical Reports Server at http://ntrs.nasa.gov, Apr. 20, 2009.

[83]. Nancy P. Sykes, ed., NASA Workshop on Computational Structural Mechanics, NASA CP-10012 (1989).

[84]. Open Channel Foundation, “AIRLOADS,” on Open Channel Foundation Web site at http://www.openchannelfoundation.org/projects/AIRLOADS, accessed May 6, 2009.

[85]. “Auto Design,” Spinoff, NASA, 1986, p. 72.

[86]. Gary L. Farley and Donald J. Baker, “Graphics and Composite Material Computer Program Enhancements for SPAR,” NASA TM-80209 (1980); and J.L. Rogers, Jr., “Programming Structural Synthesis System,” NASA Tech Briefs, vol. 10, No. 2, (May 1986).

[87]. Anees Ahmad and Lamar Hawkins, “Development of Software to Model AXAF-1 Image Quality,” NASA CR-203978 (1996), p. 1.

[88]. Cody R. Godines and Randall D. Manteufel, “Probabilistic Analysis and Density Parameter Estimation Within Nessus,” NASA CR-2002-212008 (2002).

[89]. “Structural Analysis Made NESSUSary,” Spinoff, NASA, 2005, p. 94.

[90]. John P. Gyekenyesi, “SCARE: A Post-Processor Program to MSC/NASTRAN,” abstra