Jeffrey А., Taniuti Т. (1964). Nonlinear Wave Propagation with Applications to Physics and Magneto-Hydrodynamics. - New York: Academic.

Jensen V. G. (1959). Viscous Flow Round a Sphere at Low Reynolds Number

(40). -Proc. Roy. Soc. London, Ser. A, v. 249, p. 346-366.

Jobe C. E. (1974). The Numerical Solution of the Asymptotic Equations of Trailing Edge Flow. -Technical Report AFFDL-TR-74-46, Air Force Flight Dy. namics Laboratory, Dayton, Ohio.

Jobe C. E,, Burgraff O, R. (1974). The Numerical Solution of the Asymptotic Equations of Trailing Edge Flow. - Proc. Roy. Soc. London, Ser. A, v. 340, p. 91-111.

Johnson F., Rubbert P. (1975). Advanced Panel-Type Influence Coefficient Methods Applied to Subsonic Flows. - AIAA Paper 75-50, Pasadena, California.

Johnson G. M. (1980). An Alternative Approach to the Numerical Simulation of Steady Inviscid Flow. -Proc. Seventh Int. Conf. Num. Methods Fluid Dyn., Lecture Notes in Physics, v. 141. -New York: Springer-Verlag, p. 236-241.

Jones W. R., Launder B. E. (1972). The Prediction of Laminarization with a Two-Equation Model of Turbulence. - Int. J. Heat Mass Transfer, v. 15, p. 301-314.

Karamcheti K. (1966). Principles of Ideal-Fluid Aerodynamics. - New York: Wiley.

Kays W. M. (1972). Heat Transfer to the Transpired Turbulent Boundary Layer. -Int. J. Heat Mass Transfer, v. 15, p. 1023-1044.

Kays W. M., Grawford M. E. (1980). Convective Heat and Mass Transfer. 2d ed. - New York: McGraw-Hill. [Имеется перевод 1-го изд.: Конвективный тепло- и массообмен.-М.: Энергия, 1972.]

Kays W. М., Moffat R. J. (1975). The Rehavior of Transpired Turbulent Boundary Layers. - Studies in Convection: Theory, Measurement, and Applications, v. 1. -New York: Academic, p. 223-319.

Keller H. B. (1970). A New Difference Scheme for Parabolic Problems. - Numerical Solutions of Partial Differential Equations, v. 2 (J. Bramble, ed.). New York: Academic.

Keller H. В., Cebeci T. (1972). Accurate Numerical Methods for Boundary-Layer Flows. II: Two-dimensional Turbulent Flows. - AIAA Journal, v. 10, p. 1193-1199. [Имеется перевод: Келлер, Себеси. Точный численный расчет течения в пограничном слое. II. Плоское турбулентное течение.- Ракетная техн. и космон., 1972, № 9, с. 73.]

Kentzer С. Р. (1970). Discretization of Boundary Conditions on Moving Discontinuities.- Proc. Second Int. Conf. Num. Methods Fluid Dyn., Lecture Notes in Physics, vol. 8.- New York: Springer-Verlag, p. 108-113. [Имеется перевод: Кенцер Ч. Дискретизация граничных условий на движущихся разрывах. В сб.: Численные методы в механике жидкости. - М.: Мир, 1973, с. 62-72.]

Kitchens (Jr.) С. W. Sedney R. and Gerber N. (1975). The Role of the Zone of Dependence Concept in Tree-dimensional Boundary-Layer Calculations.- Proc. AIAA 2nd Computational Fluid Dynamics Conference, Hartford, Connecticut, p. 102-112.

Klineberg J.M., Steger J. L. (1974). On Laminar Boundary Layer Separation.- AIAA Paper 74-94, Washington, D. C.

KHnksiek W. P., Pierce F. J. (1973). A Finite-Difference Solution of the Two-and Three-dimensional Incompressible Turbulent Boundary Layer Equations.-J. Fluids Engng., v. 95, p. 445-458.

Klopfer G. H., McRae D. S. (1981a). The Nonlinear Modified Equation Approach to Analyzing Finite-Difference Schemes. - AIAA Paper 81-1029, Pa о Alto, California.

Klopfer G. H., McRae D. S. (1981b). Nonlinear Analysis of the Truncation Er-

rors in Finite-Difference Schemes for the Full System of Euler Equations.--

AIAA Paper 81-0193, St. Louis, Missouri. Klunker E. (1971). Contributions to Methods for Calculating the Flow about

Thin Lifting Wings at Transenic Speeds - Analytical Expression for the

Far Field.-NASA TN D-6530. Knechtel E. D. (1959). Experimental Investigation at Transonic Speeds of Pressure Distributions over Wedge and Circular Arc Sections and Evaluation

of Perforated-Wall Interference. - NASA TN D-15. Korkegi R. H. (1956). Transition Studies and Skin-Friction Measurements on

an Insulated Flat Plate at a Mach Number of 5,8.- J. Aeronaut. Sci.,

V. 25, p. 97-192.

Kowalski E. J. (1980). Boundary-Fitted Coordinate Systems for Arbitrary Computational Regions. - Numerical Crid Generation Techniques, NASA Conference Publication 2166, p. 331-353.

Krause E. (1969). Comment on Solution of a Three-dimensional Boundary-Layer Flow with Separation*. - AIAA Journal, v. 7, p. 575-576. [Имеется перевод: Краузе. Замечания к статье «Решение задачи о трехмерном пограничном слое с отрывом». - Ракетная техн. и космон., 1969, Кя 3, с. 222.]

Kreskovsky J. P., Shamroth S. J., McDonald H. (1974). Parametric Study of Re-laminarization of Turbulent Boundary Layers on Nozzle Walls. - NASA CR-2370.

Kutler P., Lomax H. (1971). The Computation of Supersonic Flow Fields about Wing-Body Combinations by «Shock-Capturing» Finite Difference Techniques.-Proc. Second Int. Conf. Num. Methods Fluid Dyn., Lecture Notes in Physics, V. 8.- Berlin: Springer-Verlag, p. 24-29. [Имеется перевод: Кутлер П., Ломекс Г. Расчет сверхзвуковых течений около комбинации крыло - тело с помощью конечно-разностного метода «улавливания скачка».- В сб.: Численные методы механики жидкости. - М.: Мир, 1973, с. 126-134.]

Kutler Р., Warming R. F., Lomax И. (1973). Computation of Space Shuttle Flowfields using Noncentered Finite-Difference Schemes. - AIAA Journal, V. 11, p. 196-204. [Имеется перевод: Кутлер, Уорминг, Ломаке. Расчет обтекания транспортного космического корабля с использованием нецен тральных разностных схем. - Ракетная техн. и космон., 1973, № 2, с. 86.]

Kwon О. К., Pletcher R. Н. (1979). Prediction of Incompressible Separated Boundary Layers Including Viscous-Inviscid Interaction. - J. Fluids Engng., V. 101, p. 466-472. [Имеется перевод: Квон, Плетчер. Расчет несжимаемых пограничных оторвавшихся слоев с учетом вязко-невязкого взаимодействия. - Тр. Амер. о-ва ииж.-мех., сер. D. Теоретические основы инженерных расчетов, 1979, № 4, с. 171.]

Kwon О. К., Pletcher R. И. (1981). Prediction of the Incompressible Flow over a Rearward-Facing Step - Engineering Research Institute Technical Report 82019/HTL-26, Iowa State University, Ames.

Laasonen P. (1949). Ober eine Methode zur Losung der Warmeleitungsglei-chung. -Acta Math., v. 81, p. 309-317.

Larkin B. K. (1964). Some Stable Explicit Difference Approximations to the Diffusion Equation. - Math. Comput., v. 18, p. 196-202.

Launder B. E. (1979). Stress-Transport Closures: Into the Third Generation.- Proc. First Symposium on Turbulent Shear Flows. - New York: Springer-Verlag. [Имеется перевод: Лаундер Б. Е. Модели замыкания для напряжений-третье поколение. - В сб.: Турбулентные сдвиговые течения 1.- М.: Машиностроение, 1982, с. 270-279.]

Launder В. Е., Spalding D. В. (1972). Mathematical Models of Turbulence.- New York: Academic.

Launder B. E., Spalding D. B. (1974). The Numerical Computation of Turbulent Flows.-Comput. Methods Appl. Mech. Engng., v. 3, p. 269-289.

Lax P. D. (1954). Weak Solutions of Nonlinear Hyperbolic Equations and their Numerical Computatien. - Comms. Pure and Appl. Math., v. 7, p. 159-193.

Lax P. D., Wendroff B. (1960). Systems of Conservation Laws.- Comms. Pure and Appl. Math., v. 13, p. 217-237.

Leonard B. P. (1979a) A Stable and Accurate Convective Modelling Procedure Based on Quandratic Upstream Interpolation. - Comput. Methods Appl Mech. Engng., v. 19, p. 59-98.

Leonard B. P. (1979b). A Survey of Finite Differences of Opinion on Numerical Muddling of the Incomprehensible Defective Confusion Equation. - Finite Element Methods for Convective Dominated Flows, AMD, v. 34, The American Society of Mechanical Engineers.

Levine R. D. (182). Supercomputers. - Sci. American, v. 246, p. 118-135. [Имеется перевод: Левайн P. Д. Суперкомпьютеры. - В сб.: Современный компьютер. -М.: Мир, 1986, с. 9-29.]

LeBail R. С. (1972). Use of Fast Fourier Transforms for Solving Partial Differential Equations in Physics. - J. Сотр. Phys., v. 9, p. 440-465.

Li C. P. (1973). Numerical Solution of Viscous Reacting Blunt Body Flows of a Multicomponent Mixture. - AIAA Paper 73-202, Washington, D. C.

Li C. P. (1977). A Numerical Study Separated Flows Induced by Shock-Wave/ Boundary-Layer Interaction. - AIAA Paper 77-168, Los Angeles, California.

Li C. P. (1981). Application of an Implicit Technique to the Shock-Layer Flow Around General Bodies.- AIAA Paper 81-0191, St. Louis, Missuri; см. также AIAA Journal, 1982, v. 20, p. 175-183. [Имеется перевод: Ли К. П. Расчет неявным методом ударного слоя около произвольного тела. - Ракетная техн. и космон., 1982, т. 20, № 12, с. 18-29.]

Liebmann L. (1918). Die Angenaherte Ermittelung Harmonischer Funktionen und Konformer Abbildungen. - Sitzungsber., Math. Phys. Kl. Bayer. Akad. Wiss., V. 3, p. 385.

Liepmann H. W., Roshko A (1957). Elements of Gasdynamics. - New York: Wiley. [Имеется перевод: Липман Г. В., Рошко А. Элементы газовой динамики.-М.: ИЛ, 1962.]

Lighthill М. J. (1953). On Boundary Layers and Upstream Infuence. II. Supersonic Flows without Separation. - Proc. Roy. Soc. London, Ser. A, v. 217, p. 478-507.

Lighthill M. J. (1958). On Displacement Thickness. - J. Fluid Mech., v. 4, p. 383-392.

Lin T. C, Rubin S. G. (1973a). Viscous Flow over Spinning Cones at Angle of Attack. - AIAA Journal, v. 12, p. 975-985. [Имеется перевод: Лин, Рубин. Обтекание вращающихся конусов под углом атаки. - Ракетная техн. и космон., 1974, т 12, № 7, с. 117-128.]

Lin Т. С, Rubin S. G. (1973b). Viscous Flow over a Cone at Moderate Incidence: I. Hypersonic Tip Region. - Comput. Fluids, v. 1, p. 37-57.

Lin T. C, Rubin S. G. (1979). A Numerical Model for Supersonic Viscous Flow over a Slender Reentery Vehicle. - AIAA Paper 79-0205, New Orleans, Louisiana.

Lin T. C, Rubin S. G., Widhopf G. F. (1981). A Two-Layer Model for Coupled Three Dimensional Viscous and Inviscid Flow Calculations. - AIAA Paper 81-0118, St. Louis, Missouri.

Lindemuth I., Killeen J. (1973). Alternating Direction Implicit Techniques for Two Dimensional Magnetohydrodynamics Calculations. - J. Сотр. Phys., v. 13, p. 181-208.

Lock R. C. (1970). Test Cases for Numerical Methods in Two-dimensional Transonic Flows.- AGARD Report 575.

Lubard S. C, Helliwell W. S. (1973). Calculation of the Flow on a Cone at High Angle of Attack. -R & D Associates Technical Report, RDA-TR-150, Santa Monica, California.