Stephenson P. L. (1976). A Theoretical Study of Heat Transfer in Two-dimensional Turbulent Flow in a Curcular Pipe and Between Parallel and Diverging Plates. - Int. J. Heat Mass Transfer, v. 19, p. 413-423.

Stewartson K. (1974). Multistructured Boundary Layers on Flat Plates and Related Bodies. - Advances in Applied Mechanics v. 14.- New York: Academic, p. 145-239.

Stone H. L. (1968). Iterative Solution of Implicit Approximations of Multidimensional Partial Equations.- SIAM J. Numer. Anal. v. 5, p. 530-558.

Swaminathan S., Kim M. D., Lewis C. H. (1983). Three-dimensional Nonequili-brium Viscous Shock-Layer Flows over Complex Geometries. - AIAA Paper 83-0212, Reno, Nevada.

Szema K. Y., Lewis C. H. (1980). Three-dimensional Hypersonic Laminar, Transitional and/or Turbulent Shock-Layer Flows.- AIAA Paper 80-1457, Snow-mass, Colorado.

Tannehill J. C, Anderson D. A. (1980). Computation of Three dimensional Supersonic Viscous Flows in Internal Corners. - Technical Report AFWAL-TR-80-3017.

Tannehill J. C, Vigneron Y. C, Rakich J. V. (1978). Numerical Solution of Two-dimensional Turbulent Blunt Body Flows with an Impinging Shock.- AIAA Paper 78-1209, Seattle, Washington. [Имеется перевод: Таннехил Дж. К, Винерон И. К., Рэкич Дж. В. Численный расчет двумерного турбулентного течения около плохо обтекаемого тела при взаимодействии с падающей ударной волной. - Ракетная техн. и космон., 1979, т. 17, № 12, с. 13-15.]

Tannehill J. С, Hoist Т. L, Rakich J. V. (1975). Numerical Computation of Two-dimensional Viscous Blunt Body Flows with an Impinging Shock.- AIAA Paper 75-154, Pasadena, California. [Имеется перевод: Таннехил, Холст, Рэкич. Численное исследование двумерного вязкого обтекания (течения), развивающегося при взаимодействии затупленных тел с внешней ударной волной. - Ракетная техн. и космон., 1976, т. 14, JVb 2, с. 94-103.]

Tannehi 1 J. С, Venkatapathy Е., Rakich J. V. (1975). Numerical Solution of Supersonio Viscous Flow over Blunt Delta Wings. - AIAA Journal, v. 20, p. 203-210. [Имеется перевод: Таннехил Дж. К., Венкатапатхи Э., Рэкич Дж. В. Расчет сверхзвукового вязкого обтекания затупленных треугольных крыльев.-Ракетная техн. и космон., 1982, т. 20, № 3, с. 33-43.]

Taylor А. Е. (1955). Advanced Calculus. - Boston: Ginn and Company.

Telionis P. D., Tsahalis D. Th. (1976). Unsteady Turbulent Boundary Layers and Separation. - AIAA Journal, v. 14, p. 468-474. [Имеется перевод: Те-лионис, Цахалис. Нестационарные турбулентные пограничные слои и проблема отрыва. - Ракетная техн. и космон., 1976, JVb 4, с. 64.]

Telionis Р. D., Tsahalis D. Th., Werle М. J. (1973). Numerical Investigation of Unsteady Boundary-Layer Separation. - Phys. Fluids, v. 16, p. 968-973.

Thareja R., Szema K. Y., Lewis C. H. (1982). Effects of Chemical Equilibrium on Three-dimensional Viscous Shock-Layer Analysis of Hypersonic Laminar or Turbulent Flows. -AIAA Paper 82-0305, Orlando, Florida.

Thom A., Apelt C. J. (1961). Field Computations in Engineering and Physics.- Princeton, New Jersey: C. Van Nostrand.

Thomas L. H. (1949). Elliptic Problems in Linear Difference Equations over a Network. -New York: Watson Sci. Comput. Lab. Rept., Columbia University.

Thomas P. D., Lombard C. K. (1978). The Geometric Conservation Law - A Link between Finite-Difference and Finite-Volume Methods of Flow Computation on Moving Grids. -AIAA Paper 78-1208, Seattle, Washington.

Thomas P. D., Vinokur M., Bastianon R. A., Conti R. J. (1972). Numerical Solution for Three-dimensional Inviscid Supersonic Flow.- AIAA Journal, V. 10, p. 887-894. [Имеется перевод: Томас, Винокур, Бастианон, Конти.

Численный метод расчета пространственного невязкого сверхзвуковогате-чения. - Ракетная техн. и космон., 1972, № 7, с. 47.]

Thommen Н. U. (1966). Numerical Integration of the Navier-Stokes Equations - Z. Angew. Math. Phys., v. 17, p. 369-384.

Thompson J. F. (1980). Numerical Solution of Flow Problems Using Body-Fitted Coordinate Systems. - Computational Fluid Dynamics, v. 1 (W. Kollmann, ed). -Washington, D. C: Hemisphere.

Thompson J. F., Thames F. C, Mastin C. W. (1974). Automatic Numerical Generation of Body-Fitted Curvilinear Coordinate System for Field Containing any Number of Arbitrary Two-dimensional Bodies. - J. Сотр. Phys., v. 15, p. 299-319.

Thompson J. F., Thames F. C, Mastin C. W., /Shanks S. P. (1975). Use of numerically Generated Body-Fitted Coordinate Systems for Solution of the Navier-Stokes Equations. - Proc. AIAA 2nd Computational Fluid Dynamics Conference, Hartford, Connecticut, p. 68-80.

Ting L. (1965). On the Initial Conditions for Boundary Layer Equations.- J. Math. Phys., V. 44, p. 353-367.

Tsahalis D. Th. Telionis D. P. (1974). Oscillating Laminar Boundary Layers and Unsteady Separation. - AIAA Journal, v. 12, p. 1469-1475. [Имеется перевод: Осциллирующие ламинарные пограничные слои и нестационарный отрыв. - Ракетная техн. и космон., 1974, № 11, с. 17.]

van Driest Е. R. (1951). Turbulent Boundary Layer in Compressible Fluids.- J. Aeronaut. Sci., v. 18, p. 145-160.

van Driest E. R. (1952). Investigation of Laminar Boundary Layer in Compressible Fluids Using the Crocco Method. - NACA TN-2597.

van Driest E. R. (1956). On Turbulent Flow Near a Wall. - J. Aeronaut. Sci., V. 23, p. 1007-1011.

van Dyke M. (1969). Higher-Order Boundary-Layer Theory. - Annual Review of Fluid Mechanics, v. 1, Annual Reviews, Inc., Palo Alto, California, p. 265-292.

Varga R. S. (1962). Matrix Iterative Numerical Analysis. - New York: Wiley. Vigneron Y. C, Rakich J. V., Tannehill J. C. (1978a). Calculation of Supersonic

Viscous Flow over Delta Wings with Sharp Subsonic Leading Edges.-

AIAA Paper 78-1137, Seattle, Washington. Vigneron Y. C, Rakich J. V., Tannehill J. C. (1978b). Calculation of Supersonic

Viscous Flow over Delta Wings with Sharp Subsonic Leading Edges.-

NASA TM-78500.

Vinokur M. (1974). Conservation Equations of Gas-Dynamics in Curvilinear Coordinate Systems. -J. Сотр. Phys., v. 14, p. 105-125.

Viviand H. (1974). Conservative Forms of Gas Dynamics Equations. - Recherche Aerospatiale, No. 1974-1, p. 65-68.

von Neumann J, Richtmyer R. D. (1950). A Method for the Numerical Calculation of Hyperdynamic Shocks.- J. Appl. Phys., v. 21, p. 232-237.

Wachspress E. L. (1966). Iterative Solution of Elliptic Systems. - Englewood Cliffs, New Jersey: Prentice-Hall.

Wang К .С. (1971). On the Determination of the Zones of Influence and Dependence for Three-dimensional Boundary-Layer Equations.- J. Fluid Mech., V. 48, pt. 2, p. 397-404.

Wang K. C. (1972). Separation Patterns of Boundary Layer over an Inclined Body of Revolution. - AIAA Journal, v. 10, p. 1044-1050. [Имеется перевод: Уонг. Отрыв пограничного слоя при обтекании тел вращения под углом атаки. - Ракетная техн. и космон., № 8, с. 90.]

Wang К. С. (1973). Three-dimensional Laminar Boundary Layer over a Body of Revolution at Incidence, Part VI: General Methods and Results of the Case at High Incidence. - MML TR 73-02c, Martin Marietta Laboratories, Baltimore, Maryland.

Wang К. С. (1974), Boundary Layer over a Blunt Body at High Incidence with an Open-Type of Separation. - Proc. Roy. Soc. London, Ser. A, v. 340, p. 33-55.

Wang K. C. (1975). Boundary Layer over a Blunt Body at Low Incidence with Circumferential Reversed Flow. - J. Fluid Mech., v. 72, pt. 1, p. 49-65.

Warming R. F., Beam R. M. (1975). Upwind Second-Order Difference Schemes and Applications in Unsteady Aerodynamic Flow. - Proc. AIAA 2nd Computational Fluid Dynamics Conference, Hartford, Connecticut, p. 17-28.

Warming R. F., Beam R. M. (1977). On the Construction and Application of Implicit Factored Schemes for Conservation Laws. - Symposium on Computational Fluid Dynamics, New York; см. также: SIAM AMS Proceedings, v. 11, 1978, p. 85-129.

Warming R. F., Hyett B. J. (1974). The Modified Equation Approach to the Stability and Accuracy Analysis of Finite-Difference Methods.- J. Сотр. Phys., V. 14, p. 159-179.

Warming R. F., Kutler P., Lomax H. (1973). Second- and Third-Order Noncen-tered Difference Schemes for Nonlinear Hyperbolic Equations. - AIAA Journal, V. 11, p. 189-196. [Имеется перевод: Уорминг, Кутлер, Ломаке. Нецентральные разностные схемы второго и третьего порядка точности для решения нелинейных уравнений гиперболического типа. - Ракетная техн. и космон., 1973, № 2, с. 76.]

Waskiewicz J. D., Murray A. L., Lewis C. H. (1978). Hypersonic Viscous Shock-Layer Flow over a Highly Cooled Sphere. -AIAA Journal, v. 16, p. 189- 192. [Имеется перевод: Васкевич Дж. Д., Мюррей А. Л., Льюис К. X. Гиперзвуковой вязкий ударный слой около интенсивно охлажденной сферы.-Ракетная техн. и космон., 1978, т. 16, № 2, с. 123-125.]

Weinstock R. (1952). Calculus of Variations with Applications to Physics and Engineering. - New York: McGraw-Hill.

Welch J. E., Harlow F. H., Shannon J. P., Daly B. J. (1966). The MAC Method.-Los Alamos Scientific Laboratory Report LA 3425, Los Alamos. New Mexico.

Werle M. J., Bertke S. D. (1972). A Finite-Difference Method for Boundary Layers with Reverse Flow. -AIAA Journal, v. 10, p. 1250-1252.

Werle M. J., Dwoyer D. L. (1972). Laminar Hypersonic Interacting Boundary Layers: Subcritical Branching in the Strong Interaction Regime.- ARL 72-0011, Wright-Patterson Air Force Base, Dayton, Ohio.

Werle M. J., Vatsa V. N. (1974). A New Method for Supersonic Boundary Layer Separations. - AIAA Journal, v. 12, p. 1491-1497. [Имеется перевод: Уерл, Ватса. Новый метод расчета отрыва сверхзвуковых пограничных слоев.- Ракетная техн, и космон., 1974, № 11, с. 451.]

Werle М. J,, Verdon J. М. (1979). Solution for Supersonic Trailing Edges Including Separation. - AIAA Paper 79-1544, Williamsburg, Virginia.

Werle M. J., Polak A., Bertke S. D. (1973). Supersonic Boundary-Layer Separation and Reattachment - Finite-Difference Solutions. - Report No. AFL 72-12-1, Department of Aerospace Engineering, University of Cincinnati, Ohio.

White (Jr.) A. B. (1982). On the Numerical Solution of Initial/Boundary-Value Problems in One Space Dimension. - SIAM J. Numer. Anal., v. 19, p. 683-697.

White F. M. (1974). Viscous Fluid Flow. - New York: McGraw-Hill Whitham G. B. (1974). Linear and Nonlinear Waves. -New York: Wiley. [Имеется перевод: Уизем Дж. Линейные и нелинейные волны. - М.: Мир, 1977.]

Whittaker Е Т. Watson G. N. (1927). А Course in Modern Analysis, 4th ed. (reprinted 1962. Cambridge University Fress). [Имеется перевод: Уитте-