A perspective on computational algorithms for aerodynamic analysis and design

Progress in Aerospace Sciences

Volumn 37, Issue 2, 2001, Pages 197-243

  Jameson, Antony ^a  

^a 496 Lomita Mall   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; AIRFOILS; ALGORITHMS; COMPUTATIONAL FLUID DYNAMICS; FINITE DIFFERENCE METHOD; FINITE ELEMENT METHOD; FINITE VOLUME METHOD; MATHEMATICAL MODELS; OPTIMIZATION;

AIRCRAFT DESIGN;

AERODYNAMICS;

EID: 0035245857     PISSN: 03760421     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0376-0421(01)00004-5     Document Type: Review

References (208)

1. Calculation of plane steady transonic flows
2. Analysis of embedded shock waves calculated by relaxation methods
3. Iterative solution of transonic flows over airfoils and wings, including flows at Mach 1
4. Transonic potential flow calculations in conservation form
5. Artificial compressibility method for numerical solutions of the transonic full potential equation
6. h-p adaptive finite element methods for compressible and incompressible flows
7. On the numerical solution of nonlinear problems in fluid dynamics by least squares and finite element methods (II), application to transonic flow simulations
8. Finite element methods for high speed flows
9. Calculation of inviscid transonic flow over a complete aircraft
10. Improvements to the aircraft Euler method
11. Numerical simulation of 3-D hypersonic Euler flows around space vehicles using adapted finite elements
12. Multigrid solution of the Navier-Stokes equations on triangular meshes
13. Multigrid solution of compressible turbulent flow on unstructured meshes using a two-equation model
14. Comments on the feasibility of LES for wings, and on a hybrid RANS/LES approach
15. The impact of turbulence modelling on the numerical prediction of flows
16. Computation of turbulent supersonic flows around pointed bodies having crossflow separation
17. Numerical simulation of three-dimensional vortex flows over delta wing configurations
18. A mathematically simple turbulence closure model for attached and separated turbulent boundary layers
19. A comparison of the predictive capabilities of several turbulence models using upwind and centered-difference computer codes
20. Navier-Stokes calculations for transport wing-body configurations with nacelles and struts
21. The calculation of low-Reynolds-number phenomena with a two-equation model of turbulence
22. A half a century historical review of the k-ω model
23. Application of a new k-τ model to near wall turbulent flows
24. Zonal two-equation k-ω turbulence models for aerodynamic flows
25. Numerical simulation of viscous transonic airfoil flows
26. A near wall model for the k-l two equation turbulence model
27. A one-equation turbulence transport model for high Reynolds number wall-bounded flows
28. A one-equation turbulent model for aerodynamic flows
29. Renormalization group analysis of turbulence. I. Basic theory
30. On the Yakhot-Orszag renormalization group for deriving turbulence statistics and models
31. RNG-based turbulence transport approximations with applications to transonic flows
32. Naval ship superstructure design: Complex three-dimensional flows using an efficient, parallel method
33. Mesh generation by a sequence of transformations
34. A multi-surface method of coordinate generation
35. Generation of boundary-conforming grids around wing-body configurations using transfinite interpolation
36. Three-dimensional algebraic mesh generation
37. Automatic numerical generation of body-fitted curvilinear coordinate system for field containing any number of arbitrary two-dimensional bodies
38. Boundary-fitted coordinate systems for numerical solution of partial differential equations: A review
39. Elliptic generation of compressible three-dimensional grids about realistic aircraft
40. Three-dimensional elliptic grid generation for an F-16
41. Generation of body-fitted coordinates using hyperbolic partial differential equations
42. Grid generation and flow calculations for aircraft geometries
43. A numerical investigation on wing/nacelle interferences of USB configuration
44. A 3-D Chimera grid embedding technique
45. Extended Chimera grid embedding scheme with applications to viscous flows
46. Sur la sphere vide
47. Nouvelles applications des parametres continus a la theorie des formes quadratiques. Deuxieme Memoire: Recherches sur les parallelloedres primitifs
48. Cell vertex multigrid schemes for solution of the Euler equations
49. A vertex based multigrid algorithm for three-dimensional compressible flow calculations
50. An efficient cell-vertex multigrid scheme for the three-dimensional Navier-Stokes equations
51. Systems of conservation laws
52. Hyperbolic systems of conservation laws and the mathematical theory of shock waves
53. High resolution schemes for hyperbolic conservation laws
54. A difference method for the numerical calculation of discontinuous solutions of hydrodynamic equations
55. Flux vector splitting of the inviscid gas dynamic equations with applications to finite difference methods
56. Flux corrected transport, 1 SHASTA, a fluid transport algorithm that works
57. Towards the ultimate conservative difference scheme. II. Monotonicity and conservation combined in a second order scheme
58. Flux vector splitting for the Euler equations
59. Approximate Riemann solvers, parameter vectors, and difference schemes
60. Upwind difference schemes for hyperbolic systems of conservation laws
61. High resolution schemes and the entropy condition
62. High resolution schemes using flux limiters for hyperbolic conservation laws
63. A comparison of flux vector splittings for the Euler equations
64. Non-oscillatory shock capturing scheme using flux limited dissipation
65. On symmetric and upwind TVD schemes
66. A new finite element formulation for computational fluid dynamics, I, Symmetric forms of the compressible Euler and Navier-Stokes equations and the second law of thermodynamics
67. The numerical simulation of two-dimensional fluid flow with strong shocks
68. The design and application of upwind schemes on unstructured meshes
69. Higher order solution of the Euler equations on unstructured grids using quadratic reconstruction
70. Hyperbolic systems of conservation laws
71. Numerical viscosity and the entropy condition
72. Numerical viscosity and the entropy condition for conservative difference schemes
73. Riemann solvers, the entropy condition, and difference approximations
74. On the convergence of difference approximations to scalar conservation laws
75. Admissibility of difference approximations for scalar conservation laws
76. On central-difference and upwind schemes
77. Analysis and design of numerical schemes for gas dynamics 1, artificial diffusion, upwind biasing, limiters and their effect on multigrid convergence
78. Convergence to steady state solutions of the Euler equations on unstructured grids with limiters
79. Artificial diffusion, upwind biasing, limiters and their effect on accuracy and multigrid convergence in transonic and hypersonic flows
80. A new flux splitting scheme
81. A flux splitting scheme with high-resolution and robustness for discontinuities
82. Analysis and design of numerical schemes for gas dynamics 2, artificial diffusion and discrete shock structure
83. Essentially non-oscillatory shock capturing schemes of uniformly very high accuracy
84. High-order ENO schemes applied to two- and three-dimensional compressible flow
85. Efficient implementation of essentially non-oscillatory shock-capturing schemes
86. Efficient implementation of essentially non-oscillatory shock-capturing schemes II
87. Kinetic flux splitting schemes for hypersonic flows
88. A multi-dimensional kinetic-based upwind solver for the Euler equations
89. Numerical hydrodynamics from gas kinetic theory
90. Gas-kinetic finite volume methods, flux-vector splitting and artificial diffusion
91. Convection algorithms based on a diagonalization procedure for the multi-dimensional Euler equations
92. A genuinely multidimensional upwind cell-vertex scheme for the Euler equations
93. Progress in multi-dimensional upwind differencing
94. Multi-dimensional upwind schemes based on fluctuation-splitting of conservation laws
95. Multi-dimensional upwinding and multigrid
96. A review of multi-dimensional upwind residual distribution schemes for the euler equations
97. Multi-dimensional upwinding and artificial dissipation
98. Multigrid solution of the Navier-Stokes equations for flow over wings
99. Solution of steady three-dimensional compressible Euler and Navier-Stokes equations by and implicit LU scheme
100. Multigrid Navier-Stokes calculations for three-dimensional cascades
101. A hybrid adaptation method and directional viscous multigrid with prismatic-tetrahedral meshes
102. A perspective on unstructured grid flow solvers
103. Newton solution of inviscid and viscous problems
104. Newton solution of direct and inverse transonic Euler equations
105. An implicit finite difference algorithm for hyperbolic systems in conservation form
106. Implicit finite difference simulations of three-dimensional compressible flow
107. An adaptive implicit/explicit finite-element method for high speed flows
108. An implicit linelet-based solver for incompressible flows
109. Implicit schemes and LU decompositions
110. LU factorization of an implicit scheme for the compressible Navier-Stokes equations
111. Relaxation methods for unfactored implicit upwind schemes
112. Lower-upper Symmetric-Gauss-Seidel method for the Euler and Navier-Stokes equations
113. Fully conservative numerical solutions for unsteady irrotational transonic flow about airfoils
114. Multigrid algorithms for compressible flow calculations
115. Transonic flow calculations for aircraft
116. Computation of flow around wings based on the Euler equations
117. The speed of convergence of one iterative process
118. Multi-level adaptive solutions to boundary value problems
119. On the multi-grid method applied to difference equations
120. A multiple grid scheme for solving the Euler equations
121. Solution of the Euler equations by a multigrid method
122. A diagonal implicit multigrid algorithm for the Euler equations
123. Multigrid acceleration of the flux split Euler equations
124. Multigrid solution of the steady Euler equations
125. A new multigrid approach to convection problems
126. A high-resolution Euler solver based on multigrid, semi-coarsening, and defect correction
127. Analysis of a local matrix preconditioner for the 2-D Navier-Stokes equations
128. Analysis of semi-implicit preconditioners for multigrid solution of the 2-D Navier-Stokes equations
129. Algebraic smoothing analysis of multigrid methods for the 2-D compressible Navier-Stokes equations
130. Preconditioning compressible flow calculations on stretched meshes
131. Accelerating three-dimensional Navier-Stokes calculations
132. Multigrid solution of the Euler equations on unstructured and adaptive grids
133. A 3D finite-element multigrid solver for the Euler equations
134. A multigrid finite-element method for solving the two-dimensional Euler equations
135. Unstructured multigridding by volume aggregation: Current status
136. A 3D agglomeration multigrid solver for the Reynolds-averaged Navier-Stokes equations on unstructured meshes
137. Implicit time accurate solutions on unstructured dynamic grids
138. Time dependent calculations using multigrid, with applications to unsteady flows past airfoils and wings
139. A special stability problem for linear multistep methods
140. Time-acurate Navier-Stokes calculations with multigrid acceleration
141. Fully-implicit time-marching aeroelastic solutions
142. Multigrid unsteady Navier-Stokes calculations with aeroelastic applications
143. A new implicit algorithm with multigrid for unsteady incompressible flow calculations
144. Implicit method for the computation of unsteady flows on unstructured grids
145. Characteristic time stepping or local preconditioning of the Euler equations
146. Preconditioned methods for solving the incompressible and low speed equations
147. Multigrid strategies for viscous flow solvers on anisotropic unstructured meshes
148. Textbook multigrid efficiency for the steady euler equations
149. Direct numerical simulation of transition and turbulence in a spatially evolving boundary layer
150. Compact finite difference schemes with spectral-like resolution
151. Numerical analysis of spectral methods
152. Nodes, modes and flow codes
153. Automatic adaptive grid refinement for the Euler equations
154. Robust grid adaptation for complex transonic flows
155. Improved adaptive refinement strategies for the finite element aerodynamic configurations
156. Adaptive triangular meshes for compressible flow solutions
157. Finite element least squares solutions of the Euler equations using linear and quadratic approximations
158. Adaptive remeshing for three-dimensional compressible flow computations
159. Computational fluid dynamics in the design of the Northrop/McDonnell Douglas YF-23 ATF prototype
160. Euler/experimental correlations of sonic boom pressure signatures
161. Navier-Stokes predictions for the F-18 wing and fuselage at large incidence
162. Fully-nonlinear CFD techniques for ship performance analysis and design
163. Aerodynamic design via control theory
164. Automatic design of transonic airfoils to reduce the shock induced pressure drag
165. Optimum aerodynamic design via boundary control
166. Optimal shape design for aerodynamics
167. Aerodynamic design optimization using sensitivity analysis and computational fluid dynamics
168. Aerodynamic design and optimization in one shot
169. Adjoint operator approach to shape design for internal incompressible flow
170. Optimum design for drag minimizing bodies in incompressible flow
171. Optimal controls of Navier-Stokes equations
172. Aerodynamic design and optimization on unstructured grids with a continuous adjoint formulation
173. Practical 3D aerodynamic design and optimization using unstructured meshes
174. Optimum aerodynamic design using the Navier-Stokes equations
175. Aerodynamic shape optimization techniques based on control theory
176. Aerodynamic shape optimization of wing and wing-body configurations using control theory
177. Optimum aerodynamic design using the Control Theory
178. Business jet wing design using aerodynamic shape optimization
179. Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on parallel computers