Class information for: |
Basic class information |
Class id | #P | Avg. number of references |
Database coverage of references |
---|---|---|---|
8687 | 1228 | 27.4 | 36% |
Hierarchy of classes |
The table includes all classes above and classes immediately below the current class. |
Cluster id | Level | Cluster label | #P |
---|---|---|---|
18 | 4 | THERMODYNAMICS//ENERGY & FUELS//ENGINEERING, CHEMICAL | 531182 |
68 | 3 | ENGINEERING, AEROSPACE//AIAA JOURNAL//MECHANICS | 84081 |
824 | 2 | JOURNAL OF AIRCRAFT//ENGINEERING, AEROSPACE//JOURNAL OF THE AMERICAN HELICOPTER SOCIETY | 11874 |
8687 | 1 | AERODYNAMIC SHAPE OPTIMIZATION//JOURNAL OF AIRCRAFT//ADJOINT METHOD | 1228 |
Terms with highest relevance score |
rank | Term | termType | Chi square | Shr. of publ. in class containing term |
Class's shr. of term's tot. occurrences |
#P with term in class |
---|---|---|---|---|---|---|
1 | AERODYNAMIC SHAPE OPTIMIZATION | authKW | 409939 | 2% | 63% | 26 |
2 | JOURNAL OF AIRCRAFT | journal | 196184 | 17% | 4% | 214 |
3 | ADJOINT METHOD | authKW | 177669 | 4% | 16% | 46 |
4 | ONE SHOT METHOD | authKW | 167135 | 1% | 61% | 11 |
5 | PARALLEL CFD OPTIMIZAT UNIT | address | 150060 | 1% | 46% | 13 |
6 | SIMULTANEOUS PSEUDO TIMESTEPPING | authKW | 149186 | 0% | 100% | 6 |
7 | CONTINUOUS ADJOINT | authKW | 143851 | 1% | 64% | 9 |
8 | MESH DEFORMATION | authKW | 141236 | 2% | 23% | 25 |
9 | CIVIL AIRCRAFT UNIT | address | 127872 | 0% | 86% | 6 |
10 | ENGINEERING, AEROSPACE | WoSSC | 127241 | 49% | 1% | 599 |
Web of Science journal categories |
Rank | Term | Chi square | Shr. of publ. in class containing term |
Class's shr. of term's tot. occurrences |
#P with term in class |
---|---|---|---|---|---|
1 | Engineering, Aerospace | 127241 | 49% | 1% | 599 |
2 | Computer Science, Interdisciplinary Applications | 6179 | 19% | 0% | 239 |
3 | Mechanics | 4999 | 23% | 0% | 278 |
4 | Mathematics, Interdisciplinary Applications | 4805 | 14% | 0% | 178 |
5 | Engineering, General | 2849 | 12% | 0% | 147 |
6 | Physics, Fluids & Plasmas | 1399 | 9% | 0% | 107 |
7 | Mathematics, Applied | 426 | 9% | 0% | 106 |
8 | Engineering, Mechanical | 325 | 6% | 0% | 75 |
9 | Operations Research & Management Science | 259 | 4% | 0% | 46 |
10 | Physics, Mathematical | 258 | 5% | 0% | 58 |
Address terms |
Rank | Term | Chi square | Shr. of publ. in class containing term |
Class's shr. of term's tot. occurrences |
#P with term in class |
---|---|---|---|---|---|
1 | PARALLEL CFD OPTIMIZAT UNIT | 150060 | 1% | 46% | 13 |
2 | CIVIL AIRCRAFT UNIT | 127872 | 0% | 86% | 6 |
3 | CIVIL TRANSPORT TEAM | 103600 | 0% | 83% | 5 |
4 | AVIAT PROGRAM GRP | 97704 | 1% | 30% | 13 |
5 | COMPUTAT AEROSCI BRANCH | 97535 | 2% | 21% | 19 |
6 | MULTIDISCIPLINARY OPTIMIZAT BRANCH | 93598 | 1% | 47% | 8 |
7 | PL AERODYNAM | 91942 | 2% | 16% | 23 |
8 | TRANSPORT AIRCRAFT | 89507 | 0% | 60% | 6 |
9 | PROJET SINUS | 88798 | 0% | 71% | 5 |
10 | FLUID DYNAM BRANCH | 87555 | 1% | 39% | 9 |
Journals |
Rank | Term | Chi square | Shr. of publ. in class containing term |
Class's shr. of term's tot. occurrences |
#P with term in class |
---|---|---|---|---|---|
1 | JOURNAL OF AIRCRAFT | 196184 | 17% | 4% | 214 |
2 | AIAA JOURNAL | 95362 | 17% | 2% | 210 |
3 | COMPUTERS & FLUIDS | 25738 | 5% | 2% | 62 |
4 | INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS | 23162 | 6% | 1% | 69 |
5 | AEROSPACE SCIENCE AND TECHNOLOGY | 18167 | 3% | 2% | 39 |
6 | TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES | 15484 | 2% | 3% | 23 |
7 | INTERNATIONAL JOURNAL OF COMPUTATIONAL FLUID DYNAMICS | 15074 | 2% | 3% | 23 |
8 | OPTIMIZATION AND ENGINEERING | 14305 | 1% | 4% | 16 |
9 | AERONAUTICAL JOURNAL | 9145 | 2% | 2% | 24 |
10 | AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY | 5570 | 1% | 2% | 13 |
Author Key Words |
Rank | Term | Chi square | Shr. of publ. in class containing term |
Class's shr. of term's tot. occurrences |
#P with term in class |
LCSH search | Wikipedia search |
---|---|---|---|---|---|---|---|
1 | AERODYNAMIC SHAPE OPTIMIZATION | 409939 | 2% | 63% | 26 | Search AERODYNAMIC+SHAPE+OPTIMIZATION | Search AERODYNAMIC+SHAPE+OPTIMIZATION |
2 | ADJOINT METHOD | 177669 | 4% | 16% | 46 | Search ADJOINT+METHOD | Search ADJOINT+METHOD |
3 | ONE SHOT METHOD | 167135 | 1% | 61% | 11 | Search ONE+SHOT+METHOD | Search ONE+SHOT+METHOD |
4 | SIMULTANEOUS PSEUDO TIMESTEPPING | 149186 | 0% | 100% | 6 | Search SIMULTANEOUS+PSEUDO+TIMESTEPPING | Search SIMULTANEOUS+PSEUDO+TIMESTEPPING |
5 | CONTINUOUS ADJOINT | 143851 | 1% | 64% | 9 | Search CONTINUOUS+ADJOINT | Search CONTINUOUS+ADJOINT |
6 | MESH DEFORMATION | 141236 | 2% | 23% | 25 | Search MESH+DEFORMATION | Search MESH+DEFORMATION |
7 | SHAPE PARAMETERIZATION | 111886 | 0% | 75% | 6 | Search SHAPE+PARAMETERIZATION | Search SHAPE+PARAMETERIZATION |
8 | DISCRETE ADJOINT | 103590 | 1% | 42% | 10 | Search DISCRETE+ADJOINT | Search DISCRETE+ADJOINT |
9 | AERODYNAMIC OPTIMIZATION | 89495 | 1% | 30% | 12 | Search AERODYNAMIC+OPTIMIZATION | Search AERODYNAMIC+OPTIMIZATION |
10 | AIRFOIL SHAPE PARAMETERIZATION | 74593 | 0% | 100% | 3 | Search AIRFOIL+SHAPE+PARAMETERIZATION | Search AIRFOIL+SHAPE+PARAMETERIZATION |
Core articles |
The table includes core articles in the class. The following variables is taken into account for the relevance score of an article in a cluster c: (1) Number of references referring to publications in the class. (2) Share of total number of active references referring to publications in the class. (3) Age of the article. New articles get higher score than old articles. (4) Citation rate, normalized to year. |
Rank | Reference | # ref. in cl. |
Shr. of ref. in cl. |
Citations |
---|---|---|---|---|
1 | PETER, JEV , DWIGHT, RP , (2010) NUMERICAL SENSITIVITY ANALYSIS FOR AERODYNAMIC OPTIMIZATION: A SURVEY OF APPROACHES.COMPUTERS & FLUIDS. VOL. 39. ISSUE 3. P. 373 -391 | 29 | 67% | 47 |
2 | POOLE, DJ , ALLEN, CB , RENDALL, TCS , (2017) HIGH-FIDELITY AERODYNAMIC SHAPE OPTIMIZATION USING EFFICIENT ORTHOGONAL MODAL DESIGN VARIABLES WITH A CONSTRAINED GLOBAL OPTIMIZER.COMPUTERS & FLUIDS. VOL. 143. ISSUE . P. 1 -15 | 27 | 69% | 0 |
3 | LANZETTA, M , MELE, B , TOGNACCINI, R , (2015) ADVANCES IN AERODYNAMIC DRAG EXTRACTION BY FAR-FIELD METHODS.JOURNAL OF AIRCRAFT. VOL. 52. ISSUE 6. P. 1873 -1886 | 18 | 100% | 0 |
4 | POOLE, DJ , ALLEN, CB , RENDALL, TCS , (2015) METRIC-BASED MATHEMATICAL DERIVATION OF EFFICIENT AIRFOIL DESIGN VARIABLES.AIAA JOURNAL. VOL. 53. ISSUE 5. P. 1349 -1361 | 24 | 69% | 2 |
5 | MADER, CA , MARTINS, JRRA , (2012) DERIVATIVES FOR TIME-SPECTRAL COMPUTATIONAL FLUID DYNAMICS USING AN AUTOMATIC DIFFERENTIATION ADJOINT.AIAA JOURNAL. VOL. 50. ISSUE 12. P. 2809 -2819 | 23 | 74% | 9 |
6 | BIAVA, M , WOODGATE, M , BARAKOS, GN , (2016) FULLY IMPLICIT DISCRETE-ADJOINT METHODS FOR ROTORCRAFT APPLICATIONS.AIAA JOURNAL. VOL. 54. ISSUE 2. P. 735 -749 | 19 | 73% | 2 |
7 | DENG, SH , XIAO, TH , VAN OUDHEUSDEN, B , BIJL, H , (2016) A DYNAMIC MESH STRATEGY APPLIED TO THE SIMULATION OF FLAPPING WINGS.INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN ENGINEERING. VOL. 106. ISSUE 8. P. 664 -680 | 18 | 82% | 1 |
8 | TRUONG, AH , OLDFIELD, CA , ZINGG, DW , (2008) MESH MOVEMENT FOR A DISCRETE-ADJOINT NEWTON-KRYLOV ALGORITHM FOR AERODYNAMIC OPTIMIZATION.AIAA JOURNAL. VOL. 46. ISSUE 7. P. 1695 -1704 | 20 | 91% | 12 |
9 | POIRIER, V , NADARAJAH, S , (2016) EFFICIENT REDUCED-RADIAL BASIS FUNCTION-BASED MESH DEFORMATION WITHIN AN ADJOINT-BASED AERODYNAMIC OPTIMIZATION FRAMEWORK.JOURNAL OF AIRCRAFT. VOL. 53. ISSUE 6. P. 1905 -1921 | 20 | 77% | 0 |
10 | WALTHER, B , NADARAJAH, S , (2015) OPTIMUM SHAPE DESIGN FOR MULTIROW TURBOMACHINERY CONFIGURATIONS USING A DISCRETE ADJOINT APPROACH AND AN EFFICIENT RADIAL BASIS FUNCTION DEFORMATION SCHEME FOR COMPLEX MULTIBLOCK GRIDS.JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME. VOL. 137. ISSUE 8. P. - | 18 | 82% | 3 |
Classes with closest relation at Level 1 |