1968 AFOSR-IFP-Stanford Conference, v. 1, Stanford University, California, p. 375-383.

Reyhner T. A., Flugge-Lotz I. (1968). The Interaction of Shock Wave with Laminar Boundary Layer.- Int. J. Non-Linear Mech., v. 3, p. 173-199.

Reynolds A. J. (1975). The Prediction of Turbulent Prandtl and Schmidt Numbers. - Int. J. Heat and Mass Transfer, v. 18, p. 1055-1069.

Richardson L. F. (1910). The Approximate Arithmetical Solution by Finite Differences of Physical Problems Involving Differential Equations with Application to the Stress in a Masonry Dam. - Philos. Trans. Roy. Soc. London, Ser. A, v. 210, p. 307-357.

Richtmyer R. D. (1957). Difference Methods for Initial-Value Problems. - New York: Interscience Publishers.

Richtmyer R. D., Morton K. W. (1967). Difference Methods for Initial-Value Problems, 2d ed. - New York: Interscience Publishers, Wiley. [Имеется перевод: Рихтмайер P, Мортои К. Разностные методы решения краевых задач. -М.: Мир, 1972.]

Rizzi А., Eriksson L. Е. (1981). Transfinite Mesh Generation and Damped Euler Equation Algorithm for Transonic Flow around Wing-Body Configurations. - Proc. AIAA 5th Computational Fluid Dynamics Conference, Palo Alto, California, p. 43-69.

Roache P. J. (1972). Computational Fluid Dynamics. - New Mexico: Hermosa, Albuquerque. [Имеется перевод: Роуч П. Вычислительная гидродинамика.-М.: Мир, 1980.]

Roberts G. О. (1971). Computational Meshes for Boundary Layer Porblems.- Proc. Second Int., Conf Num. Methods Fluid Dyn., Lecture Notes in Physics, v. 8.- New York: Springer-Verlag, p. 171-177.

Rodi W. (1975). A Review of Experimental Data of Uniform Density Free Turbulent Boundary Layers. - Studies in Convection: Theory, Measurement, and Applications, v. 1 (B. E. Launder, ed.). -New York: Academic.

Rotta J. (1951). Statistische Theorie nichthomogener Turbulenz. - Z. Phys., v. 129, p. 547-572.

Rouleau W. Т., Osterle J. F. (1955). The Application of Finite Difference Methods to Boundary-Layer Type Flows. - J. Aeronaut. Sci., v. 22, p. 249-254.

Rubbert P. E., Saaris G. R. (1972). Review and Evaluation of a Three-dimensional Lifting Potential Flow Analysis Method for Arbitrary Configurations. - AIAA Paper 72-188, San Diego, California.

Rubesin M. W. (1976). A One-Equation Model of Turbulence for Use with the Compressible Navie-Stokes Equations. - NASA TM X-73-128.

Rubesin M. W. (1977). Numerical Turbulence Modeling. - AGARD Lecture Series No. 86 on Computational Fluid Dynamics, p. 3-1-3-37.

Rubin S. G. (1981). A Review of Marching Procedures for Parabolized Navie-Stokes Equations. - Proc. Symposium on Numerical and Physical Aspects of Aerodynamic Flows. - New York: Springer-Verlag, p. 171-186.

Rubin S. G., Harris J. E. (1975). Numerical Studies of Incompressible Viscous Flow in a Driven Cavity. -NASA SP-378.

Rubin S. G., Khosla P. K. (1981). Navier-Stokes Calculation with a Coupled Strongly Implicit Method -I, Finite-Difference Solutions. - Comput. Fluids, v. 9, p. 163-180.

Rubin S. G., Lin T C. (1971). Numerical Methods for Two- and Three-dimensional Viscous Flow Problems: Application to Hypersonic Leading Edge Equations. - Polytechnic Institute of Brooklyn, PIBAL Report 71-8. -New York: Farmingdale.

Rubin S. G., Lin T. C. (1972). A Numerical Method for Thee-dimensional Viscous Flow: Application to the Hypersonic Leading Edge. - J. Comput. Phys., v. 9, p. 339-364.

Rubin S. G., Lin A. (1980). Marching with the PNS Equations. - Proc. 22nd Israel Annual Conference on Aviation and Astronautics. Tel Aviv, Israel, p. 60-61; CM. также Isr. J. Technol., 1980, v. 18.

Rudman S., Pubin S. G. (1968). Hypersonic Viscous Flow over Slender Bodies with Sharp Leading Edges. -AIAA Journal, v. 6, p. 1883-1889. [Имеется перевод: Рудмен, Рубин. Гиперзвуковое вязкое обтекание удлиненных тел с острой передней кромкой. - Ракетная техн. и космон., 1968, № 10, с. 72.]

Русанов В. В. Разностные схемы третьего порядка для сквозного счета разрывных решений. -ДАН СССР, 1968, т. 180, с. 1303-1305.

Saffman Р. G., Wilcox D. С. (1974). Turbulence Model Predictions for Turbulent Boundary Layers.- AIAA Journal, v. 12, p. 541-546. [Имеется перевод: Сэффмен, Уилкокс. Модель турбулентности для расчета турбулентного пограничного слоя. - Ракетная техн. и космон., 1974, № 4, с. 160.]

Salas М. D. (1975). The Anatomy of Floating Shock Fitting. - Proc. AIAA 2nd Computational Fluid Dynamics Conference, Hartford, Connecticut, p. 47-54.

Salas M. D. (1979). Flow Properties for a Spherical Body at Low Supersonic Speeds, presented at the Symposium on Computers in Aerodynamics, Twenty-Fifth Anniversary of the Aerodynamics Laboratories, Polytechnic Institute of New York.

Саульев В. К. Об одном способе численного интегрирования уравнений диффузии.-ДАН СССР, 1957, т. 115, с. 1077-1079.

Schiff L. В., Steger J. L. (1979). Numerical Simulation of Steady Supersonic Viscous Flow. - AIAA Paper 79-0130, New Orleans, Louisiana. [Имеется перевод: Шифф Л. В., Стегер Дж. Л. Численный расчет стационарных сверхзвуковых вязких течений. - Ракетная техн. и космон., 1980, т. 18, No 12, с. 16-29.]

Schlichting Н. (1968). Boundary-Layer theory, 6th ed., translated by J. Ke-

stin. - New York: McGraw-Hill. [Имеется перевод: Шлихтинг Г. Теория

пограничного слоя. - М.: Наука, 1974.] Schlichting Н. (1979). Boundary-Layer Theory, 7th ed., translated by J. Ke-

stin -New York: McGraw-Hill. [Имеется перевод: Шлихтинг Г. Теория

пограничного слоя.]

Schneider G. Е., Zedan М. (1981). А Modified Strongly Implicit Procedure for the Numerical Solution of Field Problems. - Numer. Heat Transfer, v. 4, p. 1-19.

Schubauer G. В., Tchen C. M. (1959). Section В of Turbulent Flows and Heat Transfer, v. 5. - In: High Speed Aerodynamics and Jet Propulsion. - New Jersey: Princeton University Press.

Schumann U. (1980). Fast Elliptic Solvers and their Application in Fluid Dynamics. - Computational Fluid Dynamics. - Washington, D. C: Hemisphere, p. 402-430.

Schwartztrauber P. N., Sweet R. A. (1977). The Direct Solution of the Discrete Poisson Equation on a Disc. - SIAM J. Numer. Anal., v. 5, p. 900-907.

Shah R. K., London A. L. (1978). Laminar Flow Forced Convection in Ducts.- New York: Academic.

Shang J. S. (1977). An Implicit-Explicit Method for Solving the Navier-Stokes Equations.- AIAA Paper 77-646, Albuquerque, New Mexico. [Имеется ne-)евод: Шенг Дж. С. Неявно-явный метод численного решения уравнений Тавье - Стокса. - Ракетная техн. и космон., 1978, т. 16, № 5, с. 102- 109.]

Shang J. S., Hankey (Jr.) W. L. (1975). Supersonic Turbulent Separated Flows Utilizing the Navier-Stokes Equations. - Flow Separation, AGARD-CCP-168.

Shankar V. (1981). Treatment of Conical and Nonconical Supersonic Flows by an Implicit Marching Scheme Applied to the Full Potential Equation.- Proc. ASME/AIAA Conference on Computers in Flow Predictions and Fluid Dynamics Experiments, Washington, D. C, p. 163-170.

Shankar V., Chakravarthy S. (1981). An Implicit Marching Procedure for the Treatment of Supersonic Flow Fields using the Conservative Full Potential Equation. - AIAA Paper 81-1004, Palo Alto, California.

Shankar V., Osher S. (1982). An Efficient Full Potential Implicit Method Based on Characteristics for Analysis on Surepsonic Flows.- AIAA Paper 82-0974, St. Louis, Missouri.

Shapiro A. H. (1953). The Dynamics and Thermodynamics of Compressible Fluid Flow, v. 1. -New York: Ronald Press.

Sichel M. (1963). Structure of Weak Non-Hugoniot Shocks. - Phys. Fluids, v. 6, p. 653-663.

Smith R. E., Weigel B. L. (1980). Analytic and Approximate Boundary Fitted Coordinate Systems for Fluid Flow Simulation. - AIAA Paper 80-0192, Pasadena, California.

Southwell R. V. (1940). Relaxation Methods in Engineering Science. - London: Oxford University Press.

Spalding D. B. (1972). A Novel Finite-Difference Formulation for Differential Expressions Involving Both First and Second Derivatives. - Int. J. Numer. Methods Engng., v. 4, p. 551-559.

Srivastava B. N., Werle M. J., Davis R. T. (1978). Viscous Shock-Layer Solutions of Hypersonic Sphere Cones.- AIAA Journal, v. 16, p. 137-144. [Имеется перевод: Сривастава Б. Н., Верле М. Дж., Дэвис Р. Т. Решение уравнений вязкого ударного слоя для гиперзвукового течения около сферически затупленных тел. - Ракетная техн. и космон., 1978, т. 16, No 2, с.55-64.]

Srivastava В. N., Werle М. J., Davis R. Т. (1979). Numerical Solutions of Hypersonic Viscous Shock-Layer Equations. - AIAA Journal v. 17, p. 107- 110. [Имеется перевод: Сривастава Б. Н., Верле М. Дж., Дэвис Р. Т. Численное решение уравнений гиперзвукового ударного слоя. - Ракетная техн. и космон., 1979, № 1, с. 125-127.]

Steger J. L. (1977). Implicit Finite-Difference Simulation of Flow about Arbitrary Geometries with Application to Airfoils.-AIAA Paper 77-665, Albuquerque, New Mexico.

Steger J. L. (1978). Coefficient Matrices for Implicit Finite-Difference Solution of the Inviscid Fluid Conservation Law Equations. - Comput. Methods Appl. Mech. Engng., v. 13, p. 175-188.

Steger J. L. (1981). Д Preliminary Study of Relaxation Methods for the Inviscid Conservative Gasdynamics Equations using Flux Splitting. - NASA Contractor Report 3415.

Steger J. L., Kutler P. (1976). Implicit Finite-Difference Procedures for the Computation of Vortex Wakes. -AIAA Paper 76-385, San Diego, California.

Steger J. L, Sorenson R. L. (1980). Use of Hyperbolic Partial Differential Equations to Generate Body Fitted Coordinates. - Numerical Grid Generation Techniques, NASA Conference Publication 2166, p. 463-478.

Steger J. L., Warming R. F. (1979). Flux Vector Splitting of the Inviscid Gasdynamic Equations with Apppication to Finite-Difference Methods. - NASA TM D-78605.

Steinhoff J., Jameson A. (1981). Multiple Solution of the Transonic Potential Flow Equation. - Proc. AIAA 5th Computational Fluid Dynamics Conference. Palo Alto, California, p. 347-353.