Запорожец  Издания 

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излучающего гиперзвукового пограничного слоя на плоской пластине -

РТК, т 6, № 6, с 130-138 ] Силецкн, Вуртеле (Sielecki А, Wurtele М G) [1970] The numerical Integra

tion of the nonlinear shallow water equations with sloping boundaries - J

of Comput Phys.v 6, p 219-236 Силлс (Sills J A) [1969] Transformations for infinite regions and their appli

cation to flow problems - AIAA J, v 7, No 1, p 117-123 [Имеется пере

вод Преобразования бесконечных областей и их приложение к задачам

исследования течений - РТК, т 7, № 1, с 137-144] Симеонов С В [1967] Метод решения системы нелинейных уравнений потен

циального типа - ПММ, т 31, № 3, с 503-508 Симе (Sims J L) [1958] Results of the computations of supersonic flow fields

aft of circular cylindrical bodies of revolution by the method of characteris

tics - Army Ballistic Missile Agency Rep DA R 49, Redstone Arsenal, Ala

bama

Симуни Л М [1964] Численное решение некоторых задач движения вязкой жидкости - Инженерный журнал т 4, Ня 3, с 446-450

Синглтон (Singleton R Е) [1968] Lax - Wendroff difference scheme applied to the transonic airfoil problem - AGARD Conference Proc No 35

Синнотт (Smnott D И) [1960] The use of interpolation in improving finite difference solutions of ТЕМ mode structures - Dep of Supply Tech Note Pad 142, Australian Defense Sci Service, Weapons Res Establishment, Salisbury, South Australia

Скала, Гордон (Scala S M, Gordon P) [1966] Reflection of a shock wave at a surface-Phys of Fluids, v 9, June, p 1158-II66

--[1967] Solution of the time dipendent Navier - Stokes equations for the

flow around a circular cylinder - AlAA Paper No 67 221 AIAA 5th Aerospace Sciences Meeting, New York, January 23-26 1967, AIAA J 1968, v 6, No 5, p 815-822 [Имеется перевод Решение уравнений Навье - Стокса для нестационарного обтекания кругового цилиндра - РТК, т 6, № 5, с 56-657 ]

Скоглунд, Гей (Skoglund V J Gay В D) [1968] Numerical analysis of gas dynamics - Bureau of Engineering Research Progress Rep PR 85(68)S 082, Umv of New Mexico, Albuquerque

--[1969] Improved numerical techniques and solution of a separated in

teraction of an oblique shock wave and a laminar boundary layer - Bureau of Engineering Research Rep No ME4I(69)S 068 Umv of New Mexico, Albuquerque

Скоглунд, Коул (Skoglund V J, Cole J K) [1966] Numerical analysis of the interaction of an oblique shock wave and a laminar boundary layer - Bureau of Engineering Research Rep ME 23 Univ of New Mexico Albuquerque

Скоглунд, Коул Стаяно (Skoglund V J Cole J К Staiano E F) [1967] Development and verification of two dimensional numerical techniques for viscous compressible flows with shock waves - SC CR 67 2679 Sandia Lab , Albuquerque New Mexico

Скоглунд, Уоткинс (Skoglund V J Watkins С В Jr) [1971] Numerical solutions of non equilibrium reflected shock waves m air with radiation -SC-RR 71 0203, Sandia Lab Albuquerque New Mexico

Слотта, Элвин, Мерсье Терри (Slotta L S Elwin E H Mercier H T Ter ry M D) [1969] Stratified reservoir currents Parts 1 11 - Bullentin No 44, Engineeung Experiment Station Oregon State Univ Corvallis

Смагоринский Манабе Холлоуэй (Smagorinsky J Manabe S Holloway J L) [1965] Numerical results from a nine level general circulation model of the atmosphere -US Weather Bureau Monthly Weather Rev v 93 p 727

Смит Клаттер (Smith A M О Clutter D W) [1965] Machine calculation of compressible laminar boundary layers - AIAA J, v 3, No 4, p 639-647



[Имеется перевод Расчет сжимаемого ламинарного пограничного слоя на вычислительных машинах -РТК, т 3, JNfe 4, с 80-91 ]

Смит (Smith J) [1970] The coupled equation approach to the numerical solution of the biharmonic equation by finite differences - SIAM J on Numerical Analysis V 7, p 104-И I

Смит (Smith J H) [1970] Survey of three dimensional finite difference forms of heat equation - SC M 70 83, Sandia Lab , Albuquerque, New Mexico

Смит, Мак Колл (Smith R R, McCall D) [1970] Systems of hyperbolic P D E - Comm ACM, v 13, No 9, p 567-570

Смола, Мак Авой (Smola F M, McAvoy T J) [1969] The finite difference delay technique A new approach for solving certain first order partial differential equations - Massachusetts Univ, Amherst

Снедекер, Дональдсон (Snedeker R S, Donaldson С du P ) [1966] Observation of a bistable flow in a hemispherical cavity - AIAA J , v 4, No 4, p 735-736 [Имеется перевод Исследование течения с двумя устойчивыми состояниями в потусферической каверне -РТК, т 4 № 4 с 227-228]

Соби (Sobey R J) [1970] Finite difference schemes compared for wave deformation characteristics m mathematical modeling of two dimensional long wave propagation -Army Coastal Eng Res Center, Washington D С

Сон, Ханратти (Son J S, Hanratty T J) [1969] Numerical solution for the flow around a cylinder at Reynolds numbers of 40, 200 and 500 - J Fluid Mech , V 35, Part 2, p 369-386

Сондерс (Saunders L M) [1966] Numerical solution of the flow field in the throat region of a nozzle - Brown Eng Co, Tech Note BSVD P 66 TN 001

Спарк (Spurk J H) [1970] Experimental and numerical nonequilibrium fJow studies-AIAA J, v 8, No 6, p 1039-1045 [Имеется перевод Экспериментальное и численное исследование неравновесного течения - РТК, т 8 № 6 с 61-70]

Спеньер (Spanier J) [1967] Alternating direction methods applied to heat conduction problems - In Mathematical methods for digital computers, Vol II - New York John Wiley and Sons, Inc

Cneppoy, KyoK, Вернер (Sparrow E M, Quack H Boerner С I) [1970] Local nonsimilarity boundary layer solutions -AIAA J, v 8 No II, p 1936- 1942 [Имеется перевод Метод решения уравнений пограничного слоя при отсутствии локальной автомодельности - РТК, т 8 Л» 11 с 21-30]

Спикьер (Spikjer М N ) [1966] Convergence and stability of step by step methods for the numerical solution of initial value problems - Numerische Math, В 8 S 161-177

Сполдинг (Spaldmg D B) [1967] A theory of turbulent boundary layer - In-Proc Canadian Congress of Applied Mechanics, Univ of Laval, Quebec May 22-26 1967

Стеджер, Ломекс (Steger J L, Lomax H) [1971] Generalized relaxation methods applied to problems in transonic flow - In Holt [1971] [Имеется перс-вод Методы обобщенной релаксации в пртожении к задачам о тр iiicnv-ковом течении -В кн Численные методы в механике жидкостей -\\ • Мир, 1973 с 18-25] Стсигер Сепри (Steiger М Н, Sepri Р) [1965] On the solution of initial valued boundary layer flows - PIBAL Rept No 872 Polytechn Inst Brooklyn Dept of Aerospace Eng and Appl Mech Стернберг (Sternberg H M) [1970] Similarity solutions for reactive shock waves - Quart J Mech and Appl Math v 23 No I, p 77-99 Стоун (Stone H L) [1968] Iterative solution of implicit approximations of multi dimensional partial differential equations - SIAM J of Numerical Analysis v 5 No 3 p 530-558

Стоун, Брайен (Stone H L Brian P L T) [1960

convective transport problems-Amer Inst Chem Eng J,v 9, p681-

Numerical solution of



Стречков (Strelkoff Т) [1971] An exact numerical solution of the solitary

wave - In Holt [1971 Стренг (Strang W G) [1963] Accurate partial difference methods, I, Linear

Cauchy problems - Arch Rat Mech Anal, v 12 p 392-402

- [1964] Accurate partial difference methods, II, Non linear problems - Numerische Math , В 6, S 37-46

Стробридж, Xynep (Sfrawbridge D R, Hooper G T J) [1968] Numerical

solutions of the Navier - Stokes equations for axisymmetnc flows -

J Mech Eng Sci v 10, No 5, p 389-401 Стюартсон (Stewartson K) [1964] Tre theory of laminar boundary layers in

compressible fluids - Oxford Math Monographs - Oxford Clarendon

Press

Сэмюеле Черчилл (Samuels M R Churchill S W) [1967] Stability of a

fluid in a rectangular region heated from below -Amer Inst Eng J,

\ 13, No 1 p 77-86 Tafnep (Tyler L D ) [1965] Numerical solutions of the flow field produced

by a plane shock wave emerging into a crossflow -Ph D Diss, Dept

of Mech Eng, Oklahoma State Univ Stillwater

- [1968] Numerical results of blast wave propagation in tunnel intersections - SC RR 68 430, Sandia Lab , Albuquerque New Mexico

- [1971] Heuristic analysis of convective finite difference techniques - In Holt [1971]

Тайлер Цумвальт (Tyler L D, Zumwait G W) [1965] Numerical solutions of the flow field produced by a plane shock wave emerging into a cross flow - SC DC 65 1916 Sandia Lab Albuquerque New Mexico

Тайлер Эллис (Tyler L D, Ellis M A) [1970] The TSHOK code Lax version - SC TM 70 153 Sandia Lab, Albuquerque New Mexico

Таками Келлер (Takami H Keller H B) [1969] Steady t\\ о dimensional viscous flow on an incompressible fluid past a circular cylinder - In Frenkiel and Stewartson [1969]

Таркеч (Turkel E) [1974] Phase error and stability of second order methods for hyperbole problems 1 - J of Comput Phys v 15 No 2 p 226-250

Теварсон (Tewarson R P) [1969] Projection methods for solving sparse

linear systems - Computer J v 12 No 1 p 77-80 Tefiiop (Taylor D B) [1968] The calculation of steady plane supersonic gas

flows containing an arbitrarily large number of shocks -J of Comput

Phys v 3 p 27Э-290 Тейчор (Taylor P J) [1968] The stabdity of boundary conditions m the

numerical solutions of the time dependent Navier-Stokes equations -

ARC 30406 Aerospace Res Comm (England)

- [1969] A technique for treating Dinchlet conditions at inifrnity in numerical field problems - J of Comput Phys v 4 p 138-141

- [1970] The stability of the DuFort - Frankel method for the diffusion equation with boundary conditions involving space derivatives -Computer J, v 13 No I p 93-97

Тейчор (Taylor T D) [1964] Computing transient gas flows with shock waves - Phys of Fluids v 7 No 10 p 1713-1715

Тейлор MeccOH (Taylor T D Masson В S) [1970] Application of the un steady numerical method of Godunov to computation of supersonic flows past bell-shaped bodies - J of Comput Phys, v 5, p 443-454

Тейлор, Ндефо (Taylor T D Ndefo E) [1971] Computation of viscous flow in a channel by the method of splitting. - In Holt [1971] [Имеется перевод Расчет течения вязкой жидкости в канале при помощи метода рас щепления - В ки Численные методы в механике жидкостей - М Мир, 1973, с 218-229]



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