Chương 7. Những phương pháp sai phân hữu hạn hiện: một số ứng dụng chọn lọc với dòng nhớt và không nhớt
7.7 Tham khảo (cho các chương 1 -7)
1. Liepmann H.W. and Roshko A., Elements of Gasdynamics, Wiley, New York, 1957.
2. Moretti G. and Abbetf M., 'A Time-Dependent Computational Method for Blunt Body Flows', AIAA Journal, VoL 4, No. 12, December 1966, pp. 2136-2141.
3. Anderson John D. Jr., Fundamentals of Aerodynamics, 2nd Edition McGraw-Hitl, New York, 1991.
4. Anderson John D. Jr., 'Computational Fluid Dynamics-An Engineering Tool?’ in Numerical/ Laboratory Computer Methods in Fluid Dynamics (Ed. A.A. Pouring), ASME, New York, 1976, pp. i-12.
5. Graves Randolph A., 'Computational Fluid Dynamics: The Coming Revolution,' Astronautics and Aeronautics, Vol. 20, No. 3, March 1982, pp. 20-28.
6. Kopal Z., Tables of Supersonic Flow Around Cones, Dept. of Electrical Engineering, Center of Analysis, Massachusetts Institute of Technology, Cambridge, 1947.
7. Taylor G.I. and Maccoll J.W.,'The Air Pressure on a Cone Moving at High Speed,' Proceedings of the Royal Society (a), Vol. 139, 1933, p. 278.
8. Fay J.A. and Riddeli F.R., 'Theory of Stagnation Point Heat Transfer in Dissociated Air,' Journal of the Aeronautical Sciences, Vol. 25, No. 2, Feb. 1958, pp. 73- 85.
9. Blottner F.G., 'Chemical Nonequilibrium Boundary Layer,' AIAA Journal, Vol. 2, No. 2, Feb. 1964, pp. 232-239.
10. Blottnei F.G., 'Nonequilibrium Laminar Boundary-Layer Flow of Ionized Air,' AIAA Journal, Vol. 2, No. 11, Nov. 1964, pp. 1921-1927.
11. Hall H.G., Eschenroeder A.Q. and Marrone, P.V., 'Blunt-Nose Inviscid Airflows with Coupled Nonequilibrium Processes’, Journal of the Aerospace Sciences, Vol. 29, No.
9, Sept. 1962, pp. 1038-1051.
12. Chapman Dean R., 'Computational Aerodynamics Development and Outlook,' AIAA journal, Vol. 17, No. 12, Dec. 1979, pp. 1293-1313.
13. Advanced Technology Airfoil Research, NASA Conference Publications 2045, March 1978.
14. Anderson John D. Jr., Modern Compressible Flow: With Historical Perspective, 2nd Edition McGraw-Hill, New York, 1990.
15. Bird R.B., Slewart W.E, and Lightfoot E.N., Transport Phenomena, Wiley, I960.
16. Kutler P., 'Computation of Three-Dimensional, Inviscid Supersonic Flows,' in H.J. Wirz (ed.), Progress in Numerical Fluid Dynamics, Springer-Verlag, Berlin, 1975, pp. 293-374.
17. Hildebrand F.B., Advanced Calculus for Applications, Prentice-Hall, New Jersey, 1976.
18. Anderson Dale A., Tannchill John C. and Plctcher Richard H., Computational Fluid Mechanics and Heat Transfer, McGraw-Hill, New York, 1984.
19. Sullins G.A., Ajiderson J.D. Jr. and Drummond J.P., 'Numerical Investigation of Supersonic Base Flow wi Parallel Injection,' AIAA Paper No. 82-1001.
20. Sullins G.A., Numerical Investigation of Supersonic Base Flow wi Tangential Injection, M.S. Thesis, Department of Aerospace Engineering, University of Maryland, 1981.
21. Hoist T.L., 'Numerical Solution of Axisymmetric Boatlail Fields with Plume Simulators’, AIAA Paper No. 77-224, 1977.
22. Roberts B.O., 'Computational Meshes for Boundary Layer Problems', Lecture Notes in Physics, Springer-Vcrlag, New York, 1971, pp. 171-177.
23. Thompson J.F., Thames F.C. and Mastin C.W., 'Automatic Numerical Generation of Body-Fitted Curvilinear Coordinate Systems for Fields Containing Any Number of Arbitrary Two-Dimensional Bodies', Journal of Computational Physics, Vol. 15, pp. 299- 319, 1974.
24. Wright Andrew F., A Numerical Investigation of Low Reynolds Number Flow Over an Airfoil, M.S. Thesis, Department of Aerospace Engineering, University of Maryland, 1982.
25. Corda Stephen, Numerical Investigation of the Laminar, Supersonic Flow over a Rearward-Facing Step Using an Adaptive Grid Scheme, M.S. Thesis, Department of Aerospace Engineering, University of Maryland, 1982.
26. Dwyer H.A., Kee RJ. and Sanders B.R., 'An Adaptive Grid Method for Problems in Fluid Mechanics and Heat Transfer’, AIAA Paper No. 79-1464, 1979.-r '
27. Abbott I.H. and von Dcenhoff A.E., Theory of Wing Sections, McGraw-Hill Book Company, New York, 1949; also, Dover Publications, Inc., New York, 1959.
28. Hess J.L. and Smi A.M.O., 'Calculation of Potential Flow about Arbitrary Bodies’, in Progress in Aeronautical Sciences, Vol. 8 (edited by D. Kuchemanj, Pergsmon Press, New York, pp. 1-138..
29. Chow C.Y., An introduction to Computational Fluid Dynamics, John Wiley &
Sons, Inc., New York, 1979.
30. Winkelmann A.E. and Tsao C.P., 'An Experimental Study of the Flow on a Wing With a Partial Span Dropped Leading Edge,' AIAA Paper No. 81-1665, 1981.
31. Anderson John D. Jr., Corda Stephen and VanWie David M.,'Numerical Lifting Line Theory Applied to Drooped Leading-Edge Wings Below and Above Stall,' Journal of Aircraft, Vol. 17, No. 12, Dec. 1980, pp. 898-904.
32. Cho T.H. and Anderson J.D. Jr., 'Engineering Analysis of Drooped Leading-Edge Wings Near Stall,' Journal of Aircraft, Vol. 21, No. 6, June 1984, pp. 446-448.
33. Johnson J.L.Jr., Newsom W.A. and Satran, D.R., 'Full-Scale Wind Tunnel Investigation of the Effects of Wing Leading-Edge Modifications on the High Angle-of- Attack Aerodynamic Characteristics of a Low-Wing General Aviation Airplane’, AIAA Paper No. 80, 1844, 1980.
34. Ames Research Staff, 'Equations, Tables, and Charts for Compressible Flow,' N ACA Report 1135, 1953.
35. Anderson John D. Jr., 'A Time-Dependent Analysis-for Quasi-One-Dimensional Nozzle Flows with Vibrational and Chemical Nonequilibrium,' NOLTR 69-52, Naval Ordnance Laboratory, White Oak, MD, 1969.
36. Anderson John D.Jr., 'A Time-Dependent Analysis for Vibrational and Chemical Nonequilibrium Nozzle Flows,1AIAA Journal, Vol. 8, No. 3, March 1970, pp. 545-550.
37. MacCormack R.W., 'The Effect of Viscosity in Hypervelocity Impact Cratering,' AIAA Paper No. 69-354, 1969.
38. Anderson John D.Jr., Time-Dependent Solutions of Nonequilibrium Nozzle Flow- A Sequel', AIAA Journal, Vol 5, No. 12, Dec. 1970. pp. 2280-2282.
39. Hall J.G. and Russo A.L., 'Studies of Chemical Nonequilibrium in Hypersonic Nozzle Flows,' AFOSR TN 59-1090, Cornell Aeronautical Laboratory Report AD-1118-A- 6, November 1969.
40. Anderson John D.Jr., 'On Hypersonic Blunt Body Flow Fields Obtained wi a Time-Dependent Technique,' NOLTR 68-129, Naval Ordnance Laboratory, White Oak, MD, August 1968.
41. Dallospedaie Carlo L., 'A Numerical Solution for the Two-Dimensional Flowfield in an Internal Combustion Engine with Realistic Valve-Geometry,' M.S. Thesis, Department of Aerospace Engineering, University of Maryland, College Park, MD, 1978.
42. Berman H.A., Anderson J.D.Jr. and Drummond J.P., 'A Numerical Solution of the Supersonic Flow Over a Rearward Facing Step with Transverse Non-Reacting Hydrogen Injection,' AIAA Paper No. 82-1002, 1982.
43. Berman H.A., Anderson J.D.Jr., and Drummond J.P., 'Supersonic Flow over a Rearward Facing Step with Transverse Nonreacting Hydrogen Injection," AIAA Journal, Vol. 21, No. 12, December 1983, pp. 1707-1713.
44. Baldwin B.S. and Lomax H., ‘Thin Layer Approximations and Algebraic Model for Separated Turbulent Rows,' AIAA Paper 78-257,1978.
45. Kothari A.P. and Andcrson J.D.Jr., 'Flows Over Low Reynolds Number Airfoils- Compressible Navier-Stokes Numerical Solutions', AIAA Paper No. 85-0107, 1985.
46. Hetcher C.A., Computational Techniques for Fluid Dynamics, Vol. I:
Fundamental and General Techniques, Springer-Verlag, Berlin, 1988.
47. Fletcher C. A., Computational Techniques for Fluid Dynamics, Vol. II: Specific Techniques for Different Flow Categories, Springer-Verlag, Berlin, 1988.
48. Hirsch Charles, Numerical Compulation of Internal and External Flows, Vol. I:
Fundamentals of Numerical Discretization, Wiley, New York, 1988.
49. Hirsch Charles, Numerical Computation of Internal and External Flows, Vol. II:
Computational Melhods for Inviscid and Viscous Flows, Wiley, New York, 1990.
50. Hoffmann K.A., Computational Fluid Dynamics for Engineers. Engineering Education System, Austin, Tex., 1989.
51. Anderson John D.Jr., Computational Fluid Dynamics: The Basis wi Applications, McGraw-Httl, New York, 1995.