AERODYNAMIC ANALYSES REQUIRING ADVANCED COMPUTERS - Part II - Conference proceedings

Aug 20, 2026

Compilation of conference papers from the NASA Langley Research Center covering aerodynamic flow problems that require advanced computer use. The meeting, held March 4–6, 1975, presents results from recent theoretical research and organizes contributions into sessions on viscous flows, internal flows, and two- and three-dimensional configurations. Papers include studies of boundary layers, separation and reattachment, turbulence modeling, and computational methods relevant to high-speed and transonic aerodynamics. Contributions come from NASA centers, universities, and industry.

LanguageEnglish

CategoryResearch & Report

FormatPDF

Pages783

Reading Time32 h 53 min

AccessFree to download

PREFACE

INTRODUCTORY REMARKS

REMOTE ACCESS OF THE ILLIAC IV

VISCOUS FLOWS

Studies Involving Boundary-Layer Equations

TURBULENCE Modeling and Navier-Stokes Equations

INTERNAL FLOWS

TWO-DIMENSIONAL CONFIGURATIONS

COMPUTERIZED PROCEDURES FOR AIRFOIL DESIGN

A COMPUTER PROGRAM FOR THE ANALYSIS OF MULTIELEMENT AIRFOILS

—0 0063405 LOAN COPY:RE AFWL TECHNICAL KIRTLAND AFB. AERODYNAMIC ANALYSESREQUIRING ADVANCEDCOMPUTERS Part II A conference held at LANGLEY RESEARCH CENTER Hampton,Virginia March 4-6,1975 ③0S1976 Pt.2 TECH LIBRARY KAFB,NM —1 ! AERODYNAMIC ANALYSESREQUIRING ADVANCEDCOMPUTERS Part II A conference held at Langley Research Center in Hampton,Virginiaon March 4-6,1975 Prepared by Langley Research Center C i 2 9 EV o br For sale by the National Technical Information ServiceSpringfield,Virginia 22161Price一$17.25 PREFACE This compilation consists of papers presented at a conference on AerodynamicAnalyses Requiring Advanced Computers held at the NASA Langley Research Center onMarch 4-6,1975. The purpose of the conference was to present results of recent theoretical researchon aerodynamic flow problems requiring the use of advanced computers.The conferencewas divided into the following sessions:(1)Viscous Flows,(2)Internal Flows,(3)Two-Dimensional Configurations,and (4)Three-Dimensional Configurations.Papers werepresented by members of NASA Centers,Universities,and Industry. / Page intentionally left blank CONTENTS Part I* PREFACE……………………………………………………………………………………………………………………………………………………iii Cochairmen: Percy J.Bobbitt Victor L.Peterson Alfred Gessow 1.INTRODUCTORY REMARKS …………………………………………………………………………………………………1 2.REMOTE ACCESS OF THE ILLIAC IV…………………………………………………………………………………9 K.G. Stephens, Jr. VISCOUS FLOWS Studies Involving Boundary-Layer Equations Chairman:·Dennis M. Bushnell 3. CALCULATION OF THREE-DIMENSIONAL COMPRESSIBLE LAMINAR AND ·TURBULENT BOUNDARY LAYERS……………………………………………………………………………17. PREFACE ………………………………………………………………………………………………………………………………………17 Julius E.Harris AN IMPLICIT FINITE-DIFFERENCE PROCEDURE FOR SOLVING THE THREE-DIMENSIONAL COMPRESSIBLE LAMINAR, TRANSITIONAL, AND TURBULENT BOUNDARY-LAYER EQUATIONS ……………………………………19 Julius E.Harris CALCULATION OF THREE-DIMENSIONAL COMPRESSIBLE BOUNDARY LAYERS ON ARBITRARY WINGS………………………………………………………………………………41 Tuncer Cebeci, Kalle Kaups, Judy Ramsey,and Alfred Moser THREE-DIMENSIONAL COMPRESSIBLE BOUNDARY LAYERS OF REACTING GASES OVER REALISTIC CONFIGURATIONS ……………………………77 Robert M. Kendall, William S. Bonnett, Charles T.Nardo,and Michael J.Abbett 4.A NUMERICAL METHOD FOR THE PREDICTION OF HIGH-SPEED …………………………101 BOUNDARY-LAYER TRANSITION USING LINEAR THEORY …… Leslie M. Mack *Papers 1 to 22 are presented under separate cover. # 5.SOLUTIONS FOR INCOMPRESSIBLE SEPARATED BOUNDARY LAYERS INCLUDING VISCOUS-INVISCID INTERACTION……………………… James E.Carter and Stephen F.Wornom # 6.ON THE CALCULATION OF SUPERSONIC SEPARATING AND REATTACHING FLOWs……………………………………………………………………… John D. Murphy, Leroy L.Presley, and W.C.Rose # 7.ASYMPTOTIC THEORY OF TWO-DIMENSIONAL TRAILING-EDGE FLOws.177 R.E.Melnik and R. Chow 8.ANALYTICAL STUDY OF MIXING AND REACTING THREE-DIMENSIONAL SUPERSONIC COMBUSTOR FLOW FIELDS……………………………………………………… A.J.Baker,R. Clayton Rogers, and S.W.Zelazny Turbulence Modeling and Navier-Stokes Equations Chairman: Joseph G.Marvin 9.SUBGRID- OR REYNOLDS STRESS-MODELING FOR THREE-DIMENSIONAL TURBULENCE,COMPUTATIONS……………………………………… Morris W. Rubesin # 10.INFLUENCE OF EXTERNAL DISTURBANCES AND COMPRESSIBILITY ON FREE TURBULENT MIXING………………………………………………:... 341 Youn H.Oh and-Dennis M. Bushnell # 11.AN EXPERIMENTAL AND NUMERICAL INVESTIGATION OF SHOCK-WAVE INDUCED TURBULENT BOUNDARY-LAYER SEPARATION AT HYPERSONIC SPEEDS……………………………………………………………………… 377 J.G.Marvin,C.C.Horstman, M. W. Rubesin,T.J.Coakley, and M.I. Kussoy. 窥· # 12.CALCULATION OF SHOCK-SEPARATED TURBULENT BOUNDARY LAYERS ...:…………………………………………… B.S. Baldwin and W.C.Rose # 13.SIMULATION OF TURBULENT TRANSONIC SEPARATED FLOw OVER AN AIRFOIL ……………………………………………………………… 419 George S. Deiwert, John B.McDevitt, and Lionel L.Levy, Jr. # 14.AN INVESTIGATION OF SEVERAL

FAQs

What is the focus of the conference compilation?

It compiles papers presenting theoretical research results for aerodynamic flow problems that require advanced computers, organized around viscous flows, internal flows, and two- and three-dimensional configurations.

When and where was the conference held?

The conference was held at NASA Langley Research Center in Hampton, Virginia, on March 4–6, 1975.

How are the papers organized within the compilation?

The compilation divides the conference into sessions including Viscous Flows, Internal Flows, Two-Dimensional Configurations, and Three-Dimensional Configurations.

Aug 20, 2026

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