Class information for: |
Basic class information |
Class id | #P | Avg. number of references |
Database coverage of references |
---|---|---|---|
15521 | 708 | 18.2 | 22% |
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 |
15521 | 1 | INVERSE DESIGN//BALL SPINE ALGORITHM//TARGET PRESSURE DISTRIBUTION | 708 |
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 | INVERSE DESIGN | authKW | 217402 | 3% | 23% | 22 |
2 | BALL SPINE ALGORITHM | authKW | 215638 | 1% | 100% | 5 |
3 | TARGET PRESSURE DISTRIBUTION | authKW | 97036 | 0% | 75% | 3 |
4 | COMPRESSOR BLADE PROFILE | authKW | 86255 | 0% | 100% | 2 |
5 | CUBIC BOUNDARY ELEMENT | authKW | 86255 | 0% | 100% | 2 |
6 | DESIGN OPTIMUM SYST DOS | address | 86255 | 0% | 100% | 2 |
7 | FIELD BOUNDARY ELEMENTS | authKW | 86255 | 0% | 100% | 2 |
8 | FLEXIBLE STRING ALGORITHM | authKW | 86255 | 0% | 100% | 2 |
9 | QADR AERODYNAM | address | 86255 | 0% | 100% | 2 |
10 | STREAMFUNCTION COORDINATES | authKW | 86255 | 0% | 100% | 2 |
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 | 58665 | 44% | 0% | 309 |
2 | Mathematics, Interdisciplinary Applications | 2412 | 14% | 0% | 96 |
3 | Mechanics | 2100 | 19% | 0% | 138 |
4 | Engineering, General | 1694 | 12% | 0% | 86 |
5 | Computer Science, Interdisciplinary Applications | 1137 | 11% | 0% | 80 |
6 | Engineering, Mechanical | 825 | 12% | 0% | 83 |
7 | Mathematics, Applied | 637 | 13% | 0% | 92 |
8 | Physics, Fluids & Plasmas | 558 | 7% | 0% | 52 |
9 | Physics, Mathematical | 189 | 5% | 0% | 37 |
10 | Engineering, Marine | 150 | 1% | 0% | 6 |
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 | DESIGN OPTIMUM SYST DOS | 86255 | 0% | 100% | 2 |
2 | QADR AERODYNAM | 86255 | 0% | 100% | 2 |
3 | ADV COMPUAT METHODS BRANCH | 43128 | 0% | 100% | 1 |
4 | ADV DESIGN AERODYNAM | 43128 | 0% | 100% | 1 |
5 | CHEBOTAREV SCI MATH MECH | 43128 | 0% | 100% | 1 |
6 | CNRSLMFI | 43128 | 0% | 100% | 1 |
7 | COMMERCIAL AIRPLANCE GRP | 43128 | 0% | 100% | 1 |
8 | CONTROLS ECS | 43128 | 0% | 100% | 1 |
9 | DINAM FLUIDOS | 43128 | 0% | 100% | 1 |
10 | DIPARTIMENTO INGN MECCANIA IND | 43128 | 0% | 100% | 1 |
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 | AIAA JOURNAL | 71465 | 19% | 1% | 138 |
2 | JOURNAL OF AIRCRAFT | 64218 | 13% | 2% | 93 |
3 | INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES | 20567 | 2% | 3% | 16 |
4 | COMMUNICATIONS IN APPLIED NUMERICAL METHODS | 18280 | 2% | 3% | 15 |
5 | JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME | 9154 | 1% | 3% | 8 |
6 | INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS | 8628 | 5% | 1% | 32 |
7 | JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME | 6688 | 3% | 1% | 21 |
8 | INVERSE PROBLEMS IN ENGINEERING | 4818 | 1% | 3% | 4 |
9 | INVERSE PROBLEMS IN SCIENCE AND ENGINEERING | 4232 | 1% | 1% | 9 |
10 | ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN UND WELTRAUMFORSCHUNG | 3757 | 1% | 1% | 6 |
Author Key Words |
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 | HOLST, TL , (2000) TRANSONIC FLOW COMPUTATIONS USING NONLINEAR POTENTIAL METHODS.PROGRESS IN AEROSPACE SCIENCES. VOL. 36. ISSUE 1. P. 1 -61 | 72 | 60% | 14 |
2 | NIKFAR, M , ASHRAFIZADEH, A , MAYELI, P , (2015) INVERSE SHAPE DESIGN VIA A NEW PHYSICAL- BASED ITERATIVE SOLUTION STRATEGY.INVERSE PROBLEMS IN SCIENCE AND ENGINEERING. VOL. 23. ISSUE 7. P. 1138 -1162 | 21 | 84% | 1 |
3 | YIU, KFC , (1994) COMPUTATIONAL METHODS FOR AERODYNAMIC SHAPE DESIGN.MATHEMATICAL AND COMPUTER MODELLING. VOL. 20. ISSUE 12. P. 3-29 | 30 | 91% | 8 |
4 | NILI-AHMADABADI, M , HAJILOUY-BENISI, A , GHADAK, F , DURALI, M , (2010) A NOVEL 2D INCOMPRESSIBLE VISCOUS INVERSE DESIGN METHOD FOR INTERNAL FLOWS USING FLEXIBLE STRING ALGORITHM.JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME. VOL. 132. ISSUE 3. P. - | 14 | 100% | 3 |
5 | SHUMAL, M , NILI-AHMADABADI, M , SHIRANI, E , (2016) DEVELOPMENT OF THE BALL-SPINE INVERSE DESIGN ALGORITHM TO SWIRLING VISCOUS FLOW FOR PERFORMANCE IMPROVEMENT OF AN AXISYMMETRIC BEND DUCT.AEROSPACE SCIENCE AND TECHNOLOGY. VOL. 52. ISSUE . P. 181 -188 | 12 | 86% | 1 |
6 | MADADI, A , KERMANI, MJ , NILI-AHMADABADI, M , (2014) APPLICATION OF THE BALL-SPINE ALGORITHM TO DESIGN AN AXIAL-FLOW COMPRESSOR BLADE.SCIENTIA IRANICA. VOL. 21. ISSUE 6. P. 1981 -1992 | 12 | 86% | 2 |
7 | HESAMI, H , MAYELI, P , (2016) DEVELOPMENT OF THE BALL-SPINE ALGORITHM FOR THE SHAPE OPTIMIZATION OF DUCTS CONTAINING NANOFLUID.NUMERICAL HEAT TRANSFER PART A-APPLICATIONS. VOL. 70. ISSUE 12. P. 1371 -1389 | 19 | 53% | 0 |
8 | FERLAUTO, M , (2015) A PSEUDO-COMPRESSIBILITY METHOD FOR SOLVING INVERSE PROBLEMS BASED ON THE 3D INCOMPRESSIBLE EULER EQUATIONS.INVERSE PROBLEMS IN SCIENCE AND ENGINEERING. VOL. 23. ISSUE 5. P. 798 -817 | 14 | 70% | 2 |
9 | NILI-AHMADABADI, M , DURALI, M , HAJILOUY, A , (2014) A NOVEL AERODYNAMIC DESIGN METHOD FOR CENTRIFUGAL COMPRESSOR IMPELLER.JOURNAL OF APPLIED FLUID MECHANICS. VOL. 7. ISSUE 2. P. 329 -344 | 9 | 100% | 2 |
10 | NILI-AHMADABADI, M , DURALI, M , HAJILOUY-BENISI, A , GHADAK, F , (2009) INVERSE DESIGN OF 2-D SUBSONIC DUCTS USING FLEXIBLE STRING ALGORITHM.INVERSE PROBLEMS IN SCIENCE AND ENGINEERING. VOL. 17. ISSUE 8. P. 1037-1057 | 9 | 100% | 15 |
Classes with closest relation at Level 1 |