Class information for: |
Basic class information |
ID | Publications | Average number of references |
Avg. shr. active ref. in WoS |
---|---|---|---|
9724 | 1062 | 26.8 | 33% |
Classes in level above (level 2) |
ID, lev. above |
Publications | Label for level above |
---|---|---|
429 | 15725 | JOURNAL OF COMPUTATIONAL PHYSICS//INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS//COMPUTERS & FLUIDS |
Terms with highest relevance score |
Rank | Term | Type of term | Relevance score (tfidf) |
Class's shr. of term's tot. occurrences |
Shr. of publ. in class containing term |
Num. of publ. in class |
---|---|---|---|---|---|---|
1 | ROTOR FLOWS | Author keyword | 14 | 100% | 1% | 7 |
2 | CONTINUOUS ADJOINT | Author keyword | 10 | 73% | 1% | 8 |
3 | DISCRETE ADJOINT | Author keyword | 10 | 54% | 1% | 13 |
4 | AERODYNAMIC SHAPE OPTIMIZATION | Author keyword | 9 | 44% | 1% | 15 |
5 | FLUID DYNAM BRANCH | Address | 6 | 47% | 1% | 9 |
6 | ONE SHOT METHOD | Author keyword | 6 | 47% | 1% | 9 |
7 | PARALLEL CFD OPTIMIZAT UNIT | Address | 5 | 40% | 1% | 10 |
8 | MULTIDISCIPLINARY OPTIMIZAT BRANCH | Address | 5 | 47% | 1% | 8 |
9 | REDUCED SQP METHODS | Author keyword | 4 | 67% | 0% | 4 |
10 | SHAPE PARAMETERIZATION | Author keyword | 4 | 67% | 0% | 4 |
Web of Science journal categories |
Author Key Words |
Rank | Web of Science journal category | Relevance score (tfidf) |
Class's shr. of term's tot. occurrences |
Shr. of publ. in class containing term |
Num. of publ. in class |
LCSH search | Wikipedia search |
---|---|---|---|---|---|---|---|
1 | ROTOR FLOWS | 14 | 100% | 1% | 7 | Search ROTOR+FLOWS | Search ROTOR+FLOWS |
2 | CONTINUOUS ADJOINT | 10 | 73% | 1% | 8 | Search CONTINUOUS+ADJOINT | Search CONTINUOUS+ADJOINT |
3 | DISCRETE ADJOINT | 10 | 54% | 1% | 13 | Search DISCRETE+ADJOINT | Search DISCRETE+ADJOINT |
4 | AERODYNAMIC SHAPE OPTIMIZATION | 9 | 44% | 1% | 15 | Search AERODYNAMIC+SHAPE+OPTIMIZATION | Search AERODYNAMIC+SHAPE+OPTIMIZATION |
5 | ONE SHOT METHOD | 6 | 47% | 1% | 9 | Search ONE+SHOT+METHOD | Search ONE+SHOT+METHOD |
6 | REDUCED SQP METHODS | 4 | 67% | 0% | 4 | Search REDUCED+SQP+METHODS | Search REDUCED+SQP+METHODS |
7 | SHAPE PARAMETERIZATION | 4 | 67% | 0% | 4 | Search SHAPE+PARAMETERIZATION | Search SHAPE+PARAMETERIZATION |
8 | COMPLEX STEP METHOD | 4 | 75% | 0% | 3 | Search COMPLEX+STEP+METHOD | Search COMPLEX+STEP+METHOD |
9 | INCOMPLETE SENSITIVITY | 4 | 75% | 0% | 3 | Search INCOMPLETE+SENSITIVITY | Search INCOMPLETE+SENSITIVITY |
10 | STRUCTURED GRID GENERATION | 4 | 50% | 1% | 6 | Search STRUCTURED+GRID+GENERATION | Search STRUCTURED+GRID+GENERATION |
Key Words Plus |
Rank | Web of Science journal category | Relevance score (tfidf) |
Class's shr. of term's tot. occurrences |
Shr. of publ. in class containing term |
Num. of publ. in class |
---|---|---|---|---|---|
1 | DISCRETE ADJOINT | 27 | 83% | 1% | 15 |
2 | AERODYNAMIC SHAPE OPTIMIZATION | 21 | 61% | 2% | 23 |
3 | ADJOINT FORMULATION | 20 | 62% | 2% | 21 |
4 | AERODYNAMIC DESIGN | 16 | 46% | 2% | 26 |
5 | AIRFOIL DESIGN | 15 | 63% | 1% | 15 |
6 | MULTIELEMENT AIRFOIL | 12 | 86% | 1% | 6 |
7 | AERODYNAMIC DESIGN OPTIMIZATION | 7 | 56% | 1% | 9 |
8 | PROGRESSIVE OPTIMIZATION | 6 | 100% | 0% | 4 |
9 | VIBRATIONAL GENETIC ALGORITHM | 6 | 100% | 0% | 4 |
10 | MESH MOTION | 5 | 60% | 1% | 6 |
Journals |
Reviews |
Title | Publ. year | Cit. | Active references |
% act. ref. to same field |
---|---|---|---|---|
Numerical sensitivity analysis for aerodynamic optimization: A survey of approaches | 2010 | 31 | 43 | 67% |
Review and Unification of Methods for Computing Derivatives of Multidisciplinary Computational Models | 2013 | 5 | 52 | 44% |
Aerodynamic Shape Optimization Using First and Second Order Adjoint and Direct Approaches | 2008 | 14 | 36 | 67% |
Shape optimization in fluid mechanics | 2004 | 89 | 9 | 33% |
Global design optimization for aerodynamics and rocket propulsion components | 2001 | 69 | 11 | 45% |
Prediction of high lift: review of present CFD capability | 2002 | 51 | 37 | 54% |
The aerodynamic design of multi-element high-lift systems for transport airplanes | 2002 | 26 | 37 | 68% |
Adaptive aerodynamic optimization design method based on design variables space reconstruction concept | 2013 | 0 | 1 | 100% |
Layered elastic solid method for the generation of unstructured dynamic mesh | 2010 | 4 | 6 | 50% |
Aerodynamic considerations of blended wing body aircraft | 2004 | 26 | 9 | 33% |
Address terms |
Rank | Address term | Relevance score (tfidf) |
Class's shr. of term's tot. occurrences |
Shr. of publ. in class containing term |
Num. of publ. in class |
---|---|---|---|---|---|
1 | FLUID DYNAM BRANCH | 6 | 47% | 0.8% | 9 |
2 | PARALLEL CFD OPTIMIZAT UNIT | 5 | 40% | 0.9% | 10 |
3 | MULTIDISCIPLINARY OPTIMIZAT BRANCH | 5 | 47% | 0.8% | 8 |
4 | THERMAL TURBOMACHINES | 1 | 11% | 1.1% | 12 |
5 | BATTEN ENGN TECHNOL | 1 | 38% | 0.3% | 3 |
6 | CAE METHODS | 1 | 50% | 0.2% | 2 |
7 | MASS PROPERTIES EGW | 1 | 100% | 0.2% | 2 |
8 | ADV AERODYNAM | 1 | 33% | 0.3% | 3 |
9 | CC51 | 1 | 33% | 0.3% | 3 |
10 | WIND ENERGY UNIT | 1 | 33% | 0.3% | 3 |
Related classes at same level (level 1) |
Rank | Relatedness score | Related classes |
---|---|---|
1 | 0.0000276657 | CONFIGURAT AERODYNAM BRANCH//AVIAT PROGRAM GRP//CIVIL TRANSPORT TEAM |
2 | 0.0000146082 | AUTOMATIC DIFFERENTIATION//COMPUTATIONAL DIFFERENTIATION//INTERFACE CONTRACTION |
3 | 0.0000142026 | LOCAL SUPERSONIC REGIONS//INVERSE DESIGN//AEROSP PROP GRP |
4 | 0.0000114875 | CARBUNCLE PHENOMENON//SHOCK INSTABILITY//MACH UNIFORM |
5 | 0.0000092118 | SENSITIVITY EQUATION METHOD//CODE VERIFICATION//MANUFACTURED SOLUTIONS |
6 | 0.0000091404 | PSEUDOANALYTIC FUNCTION//SPECTRAL PARAMETER POWER SERIES//VEKUA EQUATION |
7 | 0.0000082833 | AV CONTROL//AVION CONTROL//ADAPTIVE WINGS |
8 | 0.0000070894 | JOURNAL OF AIRCRAFT//AEROELASTICITY//FLUTTER |
9 | 0.0000069152 | COMPUTER EXPERIMENT//COMPUTER EXPERIMENTS//LATIN HYPERCUBE DESIGN |
10 | 0.0000067472 | RADIATION DIFFUSION//NEWTON ITERATIVE METHODS//NEWTON KRYLOV METHODS |