Диссертация (1025494), страница 20
Текст из файла (страница 20)
Leonard A. Vortex Methods for Flow Simulation // J. Comput. Phys. 1980. N 37. pp.289-335.123. Lewis R.I. Vortex Element Methods for Fluid Dynamic Analysis of Engineering Systems.Cambridge: Cambridge University Press, 2005. 588 p.164124. Lorentzon, J. Fluid-structure interaction (FSI) case study of a cantilever using OpenFOAMand DEAL.II with application to VIV. Thesis for the degree of Master Science in TechnicalMathematics. Lunds Institute of Technology. Sweden. 2009. 86 p.125. Alden C. Mackey and Robert D, Schwartz. Apollo experience report the development ofdesign-loads criteria, methods, and operational and midboost conditions procedures for prelaunch,lift-off, nasa technical note nasa tn d-7373 Houston, Texas. 1973.126.
Michael P. Païdoussis, Stuart J. Price, Emmanuel de Langre. Fluid-Structure Interactions.Cross-Flow-Induced Instabilities. Cambridge University Press. 2014. 414 p.127. Morgental G. Aerodynamic Analysis of Structures Using High-resolution Vortex ParticleMethods: PhD thesis. Cambridge: University of Cambridge, Department of Engineering, 2002.209 p.128. NASA space vehicle design criteria. Prelaunch ground wind loads. NASA SP-8008(Washington, DC, United States), November,1965. p. 16.129.
Jeremy T. Pinier, Gary E. Erickson, John W. Paulson, William G. Tomek, David W.Bennett, and John A. BlevinsSpace Launch System Liftoff and Transition AerodynamicCharacterization in the NASA Langley 14by 22-Foot Subsonic Wind Tunnel // AIAA SciTech2015; 5-9 Jan. 2015. Kissimmee, FL; United States.130. Reed, Wilmer H., III.
Models for Obtaining Effects of Ground Winds in Space VehiclesErected on the Launch Pad, Presented at the Conference on the Role of Simulation in SpaceTechnology, Virginia Polytechnic Institute, Blacksburg, Virginia, August 17-21. 1964.131. Bojan Šekutkovskia, Ivan Kosti´c, Aleksandar Simonovi´c, Philip Cardiff, VladimirJazarevi´c Three-dimensional fluid–structure interaction simulation with a hybrid RANS–LESturbulence model for applications in transonic flow domain//Aerospace Science and Technology,2016.
No. 49. pp.1–16.132. Rockot User's Guide EHB0003, Issue 5, Revision 0, EUROCKOT Launch ServicesGmbHAugust2011.URL:http://www.eurockot.com/wp-content/uploads/2012/10/UsersGuideIss5Rev0web.pdf (дата обращения 30.03.2017).133. Selvi Rajan S., Santhoshkumar M., Lakshmanan, Nadaraja Pillai. S, Paramasivam M. CFDAnalysis and Wind Tunnel Experiment on a Typical Launch Vehicle Model // Tamkang Journalof Science and Engineering.
2009. Vol. 12, No. 3, pp. 223-229.165134. Spalart P.R. Strategies for turbulence modeling and simulations // International Journal ofHeat and Fluid Flow. 2000. V. 22. pp. 252–263.135. Terrestrial Environment (Climatic) Criteria Handbook for Use in Aerospace VehicleDevelopment, Pg. 2-20. NASA-HDBK-100. August 11, 2000.136. D. D. Tomlin, "Designs to Control Wind-Induced Oscillations of Launch Vehicles" (April5, 1965).The Space Congress® Proceedings. Paper 3. URL: http://commons.erau.edu/spacecongress-proceedings/proceedings-1965-2nd/session-11/3 (дата обращения 30.03.2017).137.
Thomas G. Ivanco and Donald F. Keller. Investigation of Ground-Wind Loads for AresLaunch Vehicles. Journal of Spacecraft and Rockets. Vol. 49. No. 4 (2012). pp. 574-585. DOI:10.2514/2.A32177.138. The Sixth International Conference on Computational Fluid Dynamics: Book of Abstracts.St.Petersburg, 2010. 360 p.139. Lighthill M.J. Introduction. Boundary Layer Theory // Laminar Boundary Layers / Editedby J. Rosenhead.
New-York: Oxford University Press, 1963. pp. 54-62.140. Uhlman J.S. An Integral Equation Formulation of the Equation of Motion of anIncompressible Fluid: Technical Report / Naval Undersea Warfare Center, 1996. No. 10, 086.30 p.166167.