-
2
-
-
84997303564
-
An Electrostatic Analog for Generating Cascade Grids
-
(1980)
WNGG-NASA
, pp. 129
-
-
Adamczyk1
-
3
-
-
85086289464
-
Navier-Stokes Computations of Compressible 2-D Impinging Jet Flowfields Using a Two-Equation Turbulence Model
-
Pasadena, Ca., AIAA 18th Aerospace Sciences Meeting
-
(1980)
AIAA-80-0007
-
-
Agarwal1
Bower2
-
8
-
-
84915579733
-
User's Manual for a Finite-Difference Calculation of Turbulent Swirling Compressible Flow in Axisymmetric Ducts with Struts and Slot Cooled Walls
-
(1974)
USAAMRDLTR-74-50
, vol.1
-
-
Anderson1
-
9
-
-
84915650056
-
Finite Difference Grid Generation by Multivariate Blending Function Interpolation
-
(1980)
WNGG-NASA
, pp. 143
-
-
Anderson1
Spradley2
-
10
-
-
84915608171
-
Component-Adaptive Grid Embedding
-
(1980)
WNGG-NASA
, pp. 157
-
-
Atta1
-
11
-
-
85069339755
-
Component-adaptive grid interfacing
-
AIAA 19th Aerospace Sciences Meeting, St. Louis, Mo.
-
(1981)
AIAA-81-0382
-
-
Atta1
-
12
-
-
84915615223
-
Grid and Metric Generation on the Assembly of Local BiQuadratic Coordinate Transformations
-
(1980)
WNGG-NASA
, pp. 175
-
-
Baker1
Manhardt2
-
18
-
-
84915609482
-
A High Reynolds Number Numerical Solution of the Navier-Stokes Equations in Stream Function-Vorticity Form
-
Mississippi State Univ
-
(1977)
M.S. thesis
-
-
Bearden1
-
20
-
-
85069347134
-
A Numerical Simulation of Two-Dimensional Inlet Flow Fields
-
AIAA 19th Aerospace Sciences Meeting, St. Louis, Mo.
-
(1981)
AIAA-81-0187
-
-
Birignen1
McMillan2
-
24
-
-
11644302534
-
Analysis and Computation of Viscous Subsonic Primary and Secondary Flows
-
Williamsburg, AIAA 4th Computational Fluid Dynamics Conference
-
(1979)
AIAA 79-1453
-
-
Briley1
Mcdonald2
-
28
-
-
2942683864
-
A New Boundary-Layer Inviscid Iteration Technique for Separated Flow
-
Williamsburg, AIAA 4th Computational Fluid Dynamics Conference
-
(1979)
AIAA 79-1450
-
-
Carter1
-
32
-
-
0017546704
-
Accelerated Iterative Calculation of Transonic Nacelle Flowfields
-
Washington, AIAA 14th Aerospace Sciences Meeting
-
(1976)
AIAA 76-100
-
-
Caughey1
Jameson2
-
33
-
-
84961942495
-
Inviscid Analysis of Dual-Throat Nozzle Flows
-
Palo Alto, Calif., AIAA 14th Fluid and Plasma Dynamics Conf.
-
(1981)
AIAA-81-1201
-
-
Chakravarthy1
-
35
-
-
84915633300
-
Three-Dimensional Two-Phase Supersonic Nozzle Flows
-
Palo Alto, Calif., AIAA 14th Fluid and Plasma Dynamics Conf.
-
(1981)
AIAA-81-1219
-
-
Chang1
-
38
-
-
85069341784
-
Higher-Accuracy Finite-Difference Schemes for Transonic Airfoil Flowfield Calculations
-
St. Louis, Mo., AIAA 19th Aerospace Sciences Meeting
-
(1981)
AIAA-81-0381
-
-
Chen1
-
39
-
-
84998973234
-
A Higher-Order, Finite-Difference Scheme for Transonic Flowfields Around Complex 3-D Geometries
-
Williamsburg, AIAA 4th Computational Fluid Dynamics Conference
-
(1979)
AIAA 79-1460
-
-
Chen1
Caughey2
-
40
-
-
84915633296
-
Calculation of Transonic Inlet Flowfields Using Generalized Coordinates
-
New Orleans, La., AIAA 17th Aerospace Sciences Meeting
-
(1979)
AIAA 79-0012
-
-
Chen1
Caughey2
-
42
-
-
85088228299
-
An Alternating-Direction-Implicit Algorithm for Unsteady Potential Flow
-
St. Louis, Mo., AIAA 19th Aerospace Sciences Meeting
-
(1981)
AIAA-81-0329
-
-
Chipman1
Jameson2
-
46
-
-
0020632539
-
Nonlinear Aerodynamic Modeling of Flap Oscillations in Transonic Flow—a Numerical Validation
-
St. Louis, Mo., AIAA 19th Aerospace Sciences Meeting
-
(1981)
AIAA-81-0073
-
-
Chyu1
Schiff2
-
49
-
-
85003320896
-
Computation of High Reynolds Number Internal/External Flows
-
Palo Alto, Calif., AIAA 14th Fluid and Plasma Dynamics Conf.
-
(1981)
AIAA-81-1194
-
-
Cline1
Wilmoth2
-
50
-
-
84915633292
-
Boundary-Fitted Coordinate Systems for Three-Dimensional Regions Containing Ship-Like Bodies
-
David W. Taylor Naval Ship Research and Development Center
-
(1978)
DTNSRDC-78085
-
-
Coleman1
-
51
-
-
4344609678
-
Generation of Orthogonal Boundary-Fitted Coordinate Systems
-
(1980)
WNGGNASA
, pp. 213
-
-
Coleman1
-
52
-
-
84910442329
-
NUMESH: A Computer Program to Generate Finite Difference Meshes for Arbitrary Doubly-Connected Two-Dimensional Regions
-
David W. Taylor Naval Ship Research and Development Center
-
(1977)
CMLD-77-05
-
-
Coleman1
-
54
-
-
84915633291
-
An Approximate Factorization Solution of the Navier-Stokes Equations for Transonic Flow Using Body-Fitted Coordinates with Application to NACA 64A010 Airfoils
-
Mississippi State University
-
(1980)
Ph.D. dissertation
-
-
Cooper1
-
55
-
-
84915633290
-
A Pansonic Navier-Stokes Solver
-
Palo Alto, Calif., AIAA 14th Fluid and Plasma Dynamics Conf.
-
(1981)
AIAA-81-1195
-
-
Cooper1
Thompson2
-
56
-
-
85085266620
-
Fast Navier-Stokes Solution of Transonic Flowfield about Axisymmetric Afterbodies
-
Pasadena, Calif., AIAA 18th Aerospace Sciences Meeting
-
(1980)
AIAA-80-0193
-
-
Cosner1
-
62
-
-
0013220410
-
Numerical Methods for Coordinate Generation Based on Schwarz-Christoffel Transformations
-
Williamsburg, AIAA 4th Computational Fluid Dynamics Conference
-
(1979)
AIAA 79-1463
-
-
Davis1
-
64
-
-
85003321460
-
Numerical Simulation of Three-Dimensional Boattail Afterbody Flowfields
-
(1981)
AIAA Journal
, vol.19
, pp. 582
-
-
Deiwert1
-
66
-
-
84915614604
-
Grid Generation Using Course, Smooth Finite Elements
-
(1980)
WNGG-NASA
, pp. 231
-
-
Dickson1
-
67
-
-
84915633288
-
Numerical Solution of the Biharmonic Plate Equation for Arbitrarily Shaped Plates Utilizing Automatically-Generated Boundary-Fitted Curvilinear Coordinate Systems
-
Mississippi State University
-
(1979)
M.S. thesis
-
-
Dow1
-
68
-
-
0020183353
-
Numerical Study of a Scramjet Engine Flow Field
-
St. Louis, Mo., AIAA 19th Aerospace Sciences Meeting
-
(1981)
AIAA-81-0186
-
-
Drummond1
Weidner2
-
69
-
-
84915652023
-
Fast Generation of Body Conforming Grids for 3-D Axial Turbomachinery Flow Calculations
-
(1980)
WNGG-NASA
, pp. 241
-
-
Dulikravich1
-
70
-
-
84948856578
-
Shockless Design and Analysis of Transonic Blade Shapes
-
Palo Alto, Calif., AIAA 14th Fluid and Plasma Dynamics Conf.
-
(1981)
AIAA-81-1237
-
-
Dulikravich1
Sobieczky2
-
78
-
-
84915633284
-
Three-Dimensional Coordinates About Wings
-
Williamsburg, AIAA 4th Computational Fluid Dynamics Conference
-
(1979)
AIAA 79-1461
-
-
Eiseman1
-
83
-
-
84915997146
-
Three-Dimensional Spline-Generated Coordinate Transformations for Grids Around Wing-Body Configurations
-
(1980)
WNGG-NASA
, pp. 253
-
-
Eriksson1
-
84
-
-
85086615752
-
Body-Fitted 3-D Full-Potential Flow Analysis of Complex Ducts and Inlets
-
St. Louis, Mo., AIAA 19th Aerospace Sciences Meeting
-
(1981)
AIAA-81-0002
-
-
Forester1
-
92
-
-
84915633281
-
Potential Flow about Arbitrary Biplane Wing Sections
-
(1936)
NACA TR
, pp. 542
-
-
Garrick1
-
96
-
-
85024639454
-
Boundary-Fitted Coordinates for Regions with Highly-Curved Boundaries and Reentrant Boundaries
-
(1980)
WNGG-NASA
, pp. 295
-
-
Ghia1
Ghia2
-
100
-
-
84910425163
-
An Optimization Study for Generating SurfaceOriented Coordinates for Arbitrary Bodies in High-Re Flow
-
Air Force Flight Dynamics Lab. WPAFB
-
(1977)
AFFDL-TR-77-117
-
-
Ghia1
Hodge2
Hankey3
-
105
-
-
85003380367
-
Forebody and Afterbody Solutions of the Navier-Stokes Equations for Supersonic Flow over Blunt Bodies in a Generalized Orthogonal Coordinate System
-
Langley Research Center
-
(1978)
NASA Technical Paper No. 1075
-
-
Gnoffo1
-
106
-
-
85003220661
-
A Generalized Orthogonal Coordinate System for Describing Families of Axisymmetric and Two-Dimensional Bodies
-
Langley Research Center
-
(1977)
NASA TM X-3468
-
-
Gnoffo1
-
111
-
-
85069339185
-
Navier-Stokes Solution of a Slender Body of Revolution at Large Incidence
-
St. Louis, Mo., AIAA 19th Aerospace Sciences Meeting
-
(1981)
AIAA-80-0190
-
-
Graham1
Hankey2
Shang3
-
113
-
-
84915633274
-
A Simple Numerical Orthogonal Coordinate Generator for Fluid Dynamic Applications
-
(1980)
WNGG-NASA
, pp. 307
-
-
Graves1
-
114
-
-
85003360246
-
Simple, Numerically Generated Orthogonal Coordinate System for Viscous Flow
-
(1981)
AIAA Journal
, vol.19
, pp. 2
-
-
Graves1
Hamilton2
-
115
-
-
85003461522
-
Conservative Full-Potential Calculations for Axisymmetric, Transonic Flow
-
Palo Alto, Calif., AIAA 14th Fluid and Plasma Dynamics Conf.
-
(1981)
AIAA-81-1204
-
-
Green1
-
118
-
-
84910394275
-
A Three-Dimensional Body-Fitted Coordinate System for Flow Field Calculations on Asymmetric Nose Tips
-
(1980)
WNGG-NASA
, pp. 315
-
-
Hall1
-
119
-
-
85086288613
-
Conformal-Mapping Analysis of Multielement Airfoils with Boundary-Layer Corrections
-
Pasadena, Ca., AIAA 18th Aerospace Sciences Meeting
-
(1980)
AIAA-80-0069
-
-
Halsey1
-
122
-
-
84915658752
-
Conformal Mappings of Multiply-Connected Regions onto Regions with Specified Boundary Shapes
-
(1980)
WNGG-NASA
, pp. 329
-
-
Harrington1
-
127
-
-
85069339529
-
The Numerical Solution of Incompressible Turbulent Flow Over Airfoils
-
St. Louis, Mo., AIAA 19th Aerospace Sciences Meeting
-
(1981)
AIAA81-0047
-
-
Hegna1
-
133
-
-
0019262699
-
A Fast, Conservative Algorithm for Solving the Transonic Full-Potential Equation
-
Williamsburg, AIAA 4th Computational Fluid Dynamics Conf.
-
(1979)
AIAA 79-1456
-
-
Holst1
-
138
-
-
85069344749
-
Calculation of Viscous, Sonic Flow Over Hemisphere-Cylinder at 19 Degree Incidence: The Capturing of Nose Vortices
-
St. Louis, Mo., AIAA 19th Aerospace Sciences Meeting
-
(1981)
AIAA-81-0189
-
-
Hsieh1
-
139
-
-
85085666992
-
Numerical Investigation of Flowfield about a Series of Indented Nosetips
-
St. Louis, Mo., AIAA 19th Aerospace Sciences Meeting
-
(1981)
AIAA-810077
-
-
Hsieh1
-
142
-
-
0016984739
-
A Modern Look at Conformal Mapping, Including Doubly Connected Regions
-
Hartford, Conn., AIAA 8th Fluid and Plasma Dynamics Conference
-
(1975)
AIAA 75-842
-
-
Ives1
-
144
-
-
0018506357
-
Second Order Accurate Calculation of Transonic Flow Over Turbomachinery Cascades
-
Seattle, AIAA 11th Fluid and Plasma Dynamics Conference
-
(1978)
AIAA 78-1149
-
-
Ives1
Liutermoza2
-
148
-
-
84911236179
-
VAHM-A Vertically Averaged Hydrodynamic Model Using Boundary-Fitted Coordinates
-
U.S. Army Engineer Waterways Experiment Station, Vicksburg, Miss
-
(1980)
Misc. Paper HL-80-3
-
-
Johnson1
-
149
-
-
0006974243
-
A Discussion of Boundary-Fitted Coordinate Systems and Their Applicability to the Numerical Modeling of Hydraulic Problems
-
U.S. Army Engineer Waterways Experiment Station, Vicksburg, Miss
-
(1978)
Misc. Paper H-78-9
-
-
Johnson1
Thompson2
-
152
-
-
85069341631
-
Three-Dimensional Viscous Flowfield Computations in a Streamline Coordinate System
-
St. Louis, Mo., AIAA 19th Aerospace Sciences Meeting
-
(1981)
AIAA-81-0401
-
-
Kim1
Thareja2
Lewis3
-
153
-
-
85069342119
-
Calculations of Transonic Flow About an Airfoil in a Wind Tunnel
-
Snowmass, AIAA 13th Fluid and Plasma Dynamics Conference
-
(1980)
AIAA-80-1366
-
-
King1
Johnson2
-
154
-
-
85069360843
-
A Calculation Method for Multielement Airfoils in Subsonic and Transonic Potential Flow
-
Pasadena, Calif, AIAA 18th Aerospace Sciences Meeting
-
(1980)
AIAA 80-0340
-
-
Klevenhusen1
-
160
-
-
84910400247
-
Boundary-Fitted Coordinate Systems for Arbitrary Computational Regions
-
(1980)
WNGG-NASA
, pp. 331
-
-
Kowalski1
-
161
-
-
84997059395
-
Numerical Simulation for the Design of a Supersonic Cruise Nozzle with Fluid Noise Shield
-
Palo Alto, Calif., AIAA 14th Fluid and Plasma Dynamics Conf.
-
(1981)
AIAA-81-1218
-
-
Kowalski1
Peery2
Klees3
-
162
-
-
85087232003
-
Numerical Analysis of the Scramjet Inlet Flow Field Using Two-Dimensional Navier-Stokes Equations
-
St. Louis, Mo., AIAA 19th Aerospace Sciences Meeting
-
(1981)
AIAA-81-0185
-
-
Kumar1
-
164
-
-
84893407250
-
Supersonic Flow Over Ablated Nosetips Using an Unsteady Implicit Numerical Procedure
-
Huntsville, Ala., AIAA 16th Aerospace Sciences Meeting
-
(1978)
AIAA 78-213
-
-
Kutler1
Chakravarthy2
Lombard3
-
165
-
-
84915663911
-
Numerical Solution of the Compressible Navier-Stokes Equations Using Density Gradients as Additional Dependent Variables
-
Mississippi State Univ
-
(1977)
M.S. thesis
-
-
Kwon1
-
167
-
-
85003394743
-
Comment on "Potential Flow Analysis of Multielement Airfoils Using Conformal Mapping"
-
(1981)
AIAA Journal
, vol.19
, pp. 830
-
-
Laura1
-
173
-
-
0019268257
-
A Three-Dimensional Turbulent Compressible Subsonic Duct Flow Analysis for Use with Constructed Coordinate Systems
-
Snowmass, AIAA 13th Fluid and Plasma Dynamics Conf.
-
(1980)
AIAA-80-1398
-
-
Levy1
McDonald2
Bailey3
Kreskovsky4
-
176
-
-
85006235391
-
Forebody and Base Region Red-Gas Flow in Severe Planetary Entry by a Factored Implicit Numerical Method—Part I (Computational Fluid Dynamics)
-
Pasadena, Calif., AIAA 18th Aerospace Sciences Meeting
-
(1980)
AIAA-80-0065
-
-
Lombard1
Davy2
Green3
-
178
-
-
84915633251
-
Two-Body Coordinate System Generation Using Body-Fitted Coordinate System and Complex Variable Transformation
-
Mississippi State Univ
-
(1977)
M.S. thesis
-
-
Long1
-
187
-
-
84910423266
-
Three-Dimensional Body-Fitted Coordinate Systems for Numerical Solution of the Navier-Stokes Equations
-
Seattle, AIAA 11th Fluid and Plasma Dynamics Conference
-
(1978)
AIAA 78-1147
-
-
Mastin1
Thompson2
-
192
-
-
84910388183
-
Computational Fluid Dynamic Aspects of Internal Flows
-
Williamsburg, AIAA 4th Computational Fluid Dynamics Conference
-
(1979)
AIAA 79-1445
-
-
McDonald1
Bailey2
-
193
-
-
3342969258
-
FORTRAN Program for Generating a Two-Dimensional Orthogonal Mesh Between Two Arbitrary Boundaries
-
Langley Research Center
-
(1972)
NASA TN D-6766
-
-
McNally1
-
199
-
-
0019028641
-
Direct Control of the Grid Point Distribution in Meshes Generated by Elliptic Equations
-
Williamsburg, AIAA 4th Computational Fluid Dynamics Conference
-
(1979)
AIAA 79-1462
-
-
Middlecoff1
Thomas2
-
205
-
-
84915609302
-
Grid Generation Using Classical Techniques
-
(1980)
WNGG-NASA
, pp. 1
-
-
Moretti1
-
209
-
-
84998674126
-
Navier-Stokes Computations for Conventional and Hollow Projectile Shapes at Transonic Velocities
-
Palo Alto, Calif., AIAA 14th Fluid and Plasma Dynamics Conf.
-
(1981)
AIAA-81-1262
-
-
Nietubicz1
-
212
-
-
84915633243
-
An Analytical Transformation Technique for Generating Uniformly Spaced Computational Mesh
-
(1980)
WNGG-NASA, 385
-
-
Oh1
-
217
-
-
0018925217
-
Optimal Nodal Point Distribution for Improved Accuracy in Comp. Fluid Dynamics
-
New Orleans, La., AIAA 17th Aerospace Sciences Meeting
-
(1979)
AIAA 79-0272
-
-
Pierson1
Kutler2
-
221
-
-
0018984826
-
Implicit Finite-Difference Simulations of Three-Dimensional Compressible Flow
-
(1980)
AIAA Journal
, vol.18
, pp. 159
-
-
Pulliam1
Steger2
-
222
-
-
0042393144
-
Numerical Experiments in Conformal Mapping by the Method of Orthonormal Polynomials
-
(1966)
Journal of the ACM
, vol.13
, pp. 296
-
-
Rabinowitz1
-
223
-
-
85069339193
-
Application of Adaptive Grids to Fluid Flow Problems with Asymptotic Solutions
-
St. Louis, Mo., AIAA 19th Aerospace Sciences Meeting
-
(1981)
AIAA-81-0114
-
-
Rai1
Anderson2
-
226
-
-
85002526916
-
Navier-Stokes Calculations for Laminar and Turbulent Hypersonic Flow Over Indented Nosetips
-
Huntsville, Ala., AIAA 16th Aerospace Sciences Meeting
-
(1978)
AIAA 78-260
-
-
Rakich1
Vigneron2
Tannehill3
-
227
-
-
85003258835
-
Numerical Solution of Incompressible Navier-Stokes Equations in the Integro-Differential Formulation Using Boundary-Fitted Coordinate Systems
-
Albuquerque N.M., AIAA 3rd Computational Dynamics Conference
-
(1977)
AIAA 77-650
-
-
Reddy1
Thompson2
-
229
-
-
78349237645
-
Computation of Hypersonic Viscous Flow Around Three-Dimensional Bodies at High Angles of Attack
-
Palo Alto, Calif., AIAA 14th Fluid and Plasma Dynamics Conf.
-
(1981)
AIAA-81-1261
-
-
Rizk1
Chaussee2
McRae3
-
232
-
-
0020189614
-
The Strongly Implicit Procedure Applied to the Flow Field of Transonic Turbine Cascades
-
St. Louis, Mo., AIAA 19th Aerospace Sciences Meeting
-
(1981)
AIAA-81-0211
-
-
Roach1
Sankar2
-
233
-
-
84915633234
-
The Spline-Euler System, Manifold Mapping of Multiple Airfoils a Proposed Treatment of the Interface Problems
-
Aerodynamics Dept., British Aircraft Corp., Ltd
-
(1977)
Aero Report MA 37
-
-
Roberts1
-
237
-
-
85069341734
-
A Strongly Implicit Procedure for Steady Three-Dimensional Transonic Potential Flows
-
St. Louis, Mo., AIAA 19th Aerospace Sciences Meeting
-
(1981)
AIAA-81-0385
-
-
Sankar1
Malone2
Tassa3
-
241
-
-
0019231357
-
The Prediction of the Turbulent Flow Field about an Isolated Airfoil
-
Williamsburg, AIAA 12th Fluid and Plasma Dynamics Conference
-
(1979)
AIAA 79-1543
-
-
Shamroth1
Gibeling2
-
242
-
-
85069341372
-
A Navier-Stokes Solution for Laminar and Turbulent Flow Through a Cascade of Airfoils
-
Snowmass, AIAA 13th Fluid and Plasma Dynamics Conference
-
(1980)
AIAA-80-1426
-
-
Shamroth1
Gibeling2
McDonald3
-
243
-
-
85085266786
-
Numerical Simulation of Wing-Fuselage Interference
-
St. Louis, Mo., AIAA 19th Aerospace Sciences Meeting
-
(1981)
AIAA-81-0048
-
-
Shang1
-
247
-
-
0019286292
-
Numerical Solution of the Navier-Stokes Equations for a Family of Three-Dimensional Corner Geometries
-
Snowmass, AIAA 13th Fluid and Plasma Dynamics Conf.
-
(1980)
AIAA 80-1349
-
-
Smith1
-
248
-
-
84915614476
-
Two-boundary Grid Generation for the Solution of the Three-dimensional Compressible Navier-Stokes Equations
-
Langley Research Center
-
(1981)
NASA TM 83123
-
-
Smith1
-
249
-
-
85069361656
-
Analytic and Approximate Boundary Fitted Coordinate Systems for Fluid Flow Simulation
-
Pasadena, Calif., AIAA 18th Aerospace Sciences Meeting
-
(1980)
AIAA-80-0192
-
-
Smith1
Weigel2
-
250
-
-
84915633226
-
Generation of C-type Cascade Grids for Viscous Flow Computation
-
(1980)
WNGG-NASA, 437
-
-
Sockol1
-
251
-
-
0343960784
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253
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257
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260
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264
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Snowmass, AIAA 13th Fluid and Plasma Dynamics Conference
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AIAA-80-1427
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268
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AIAA-81-1217
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280
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Williamsburg, AIAA 4th Computational Fluid Dynamics Conference
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AIAA 79-1447
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Mississippi State Univ
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295
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Mississippi State Univ
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298
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AIAA-81-1290
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299
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Seattle, AIAA 11th Fluid and Plasma Dynamics Conf.
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AIAA 78-1137
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301
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On one-Dimensional Stretching Functions for Finite-Difference Calculations
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NASA CR 3313
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302
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Rutgers Univ. of N. J
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A Numerical Method for Computing Three-Dimensional Viscous Supersonic Flow Fields About Slender Bodies
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315
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Machine Solutions of Partial Differential Equations in the Numerically Generated Coordinate Systems
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Mississippi State Univ
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318
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Mississippi State Univ
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MSSUEIRS-ASE-80-6
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319
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Some Complex Numerical Integrations of the Schwarz-Christoffel Transformation and Application to Potential Flow
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Oregon State Univ
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320
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A Method for Orthogonalizing Meshes in Plane Regions, and Its Application to Discrete Fluid Mechanics Problem
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Imp. College of Science and Tech, London
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St. Louis, Mo., AIAA 19th Aerospace Sciences Meeting
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AIAA-810046
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A Numerical Study of Viscous Flow Around an Airfoil
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San Diego, AIAA 9th Fluid and Plasma Dynamics Conf.
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AIAA 76337
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334
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Calculation of Stress Concentration Factors in Uniform and Non-Uniform Shafts Utilizing Numerical Coordinate Transformation
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Mississippi State Univ
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335
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Grid Generation and Transonic Flow Calculations for Three-Dimensional Configurations
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Snowmass, AIAA 13th Fluid and Plasma Dynamics Conf.
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AIAA-80-1391
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336
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Transonic Flow Simulations for Complex Configurations with Surface Fitted Grids
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Palo Alto, Calif., AIAA 14th Fluid and Plasma Dynamics Conf.
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