Introduction
This report provides a comprehensive analytics report of the publisher American Institute of Aeronautics and Astronautics (AIAA) including basic bibliometric information, citation data, impact metrics, top journals, publication keywords, etc., over recent years. The Crossref database (up to the end of 2021) processed by ScienceGate has been used for this report as the source of data.
American Institute of Aeronautics and Astronautics (AIAA) has published 275374 documents so far, receiving a total of 1494826 citations. These numbers are equal to 0.22% and 0.14% of the total documents and citations in the scientific community, respectively. American Institute of Aeronautics and Astronautics (AIAA) has a score of 5.43 as a number of citations per document based on all recorded data. There are different types of documents published by American Institute of Aeronautics and Astronautics (AIAA). In this regard, Journal Article, Chapter, Proceedings Article, Other, Book, Monograph, and Proceedings a with the total document number of 77654, 8009, 187843, 44, 113, 514, and 1197 have the largest share, respectively. These numbers are equal to 28.20%, 2.91%, 68.21%, 0.02%, 0.04%, 0.19%, and 0.43% of the total documents published in American Institute of Aeronautics and Astronautics (AIAA) so far, respectively. American Institute of Aeronautics and Astronautics (AIAA) has been an active publisher from 1930-2021.
Basic Bibliometric Information
This section provides the bibliometrics data of American Institute of Aeronautics and Astronautics (AIAA) over the last 11 years, including the number of published documents, total citations, citations per document, and scaled number of citations per document by year. Share of American Institute of Aeronautics and Astronautics (AIAA) documents and citations among all published scientific documents are also presented here. American Institute of Aeronautics and Astronautics (AIAA) has the highest annual number of publications in 2010, with 7407 published documents. Most annual citations are also received in 2010, with 41622 citations. The highest citations per document’s scores, scaled by the number of years ahead, are associated with 2020, with scores of 0.34.
Year | Documents | Citations | Citations/Documents | Average Citations/Documents | Documents Share | Citations Share |
---|---|---|---|---|---|---|
2010 | 7407 | 41622 | 5.6193 | 0.5108 | 0.0021 | 0.0010 |
2011 | 6726 | 34881 | 5.1860 | 0.5186 | 0.0018 | 0.0009 |
2012 | 6865 | 31913 | 4.6487 | 0.5165 | 0.0017 | 0.0008 |
2013 | 6284 | 29485 | 4.6921 | 0.5865 | 0.0014 | 0.0008 |
2014 | 5565 | 27225 | 4.8922 | 0.6989 | 0.0012 | 0.0008 |
2015 | 5970 | 24259 | 4.0635 | 0.6772 | 0.0012 | 0.0008 |
2016 | 6608 | 22490 | 3.4035 | 0.6807 | 0.0013 | 0.0008 |
2017 | 6126 | 19010 | 3.1032 | 0.7758 | 0.0011 | 0.0008 |
2018 | 7014 | 13728 | 1.9572 | 0.6524 | 0.0012 | 0.0008 |
2019 | 6225 | 7383 | 1.1860 | 0.5930 | 0.0010 | 0.0008 |
2020 | 5566 | 1917 | 0.3444 | 0.3444 | 0.0008 | 0.0006 |
Document Types
There are different types of documents published by publishers. In this section, the yearly publication data of American Institute of Aeronautics and Astronautics (AIAA) are presented by document type, including Proceeding Articles, Journal Articles, Chapters, Proceedingss, Monographs, and Books.
The number of published documents by American Institute of Aeronautics and Astronautics (AIAA) are 187843, 77654, 8009, 1197, 514, and 113 for Proceeding Articles, Journal Articles, Chapters, Proceedingss, Monographs, and Books, respectively. These numbers are equal to 2.66%, 0.08%, 0.05%, 2.27%, 0.09%, and 0.01% of the whole published Proceeding Articles, Journal Articles, Chapters, Proceedingss, Monographs, and Books in the database so far, respectively.
The number of received citations by Proceeding Articles, Journal Articles, Chapters, Proceedingss, Monographs, and Books of American Institute of Aeronautics and Astronautics (AIAA) are 479253, 998966, 3579, 536, 11622, and 868, respectively. These numbers are equal to 2.67%, 0.09%, 0.02%, 5.12%, 0.21%, and 0.01% of the citations received by whole Proceeding Articles, Journal Articles, Chapters, Proceedingss, Monographs, and Books of the database so far, respectively.
The h-index value for published Proceeding Articles, Journal Articles, Chapters, Proceedingss, Monographs, and Books by American Institute of Aeronautics and Astronautics (AIAA) are 101, 247, 17, 8, 50, and 8, respectively. The corresponding values for the whole data of the database are 615, 3201, 588, 25, 760, and 793, respectively.
The g-index value for published Proceeding Articles, Journal Articles, Chapters, Proceedingss, Monographs, and Books by American Institute of Aeronautics and Astronautics (AIAA) are 15, 27, 6, 4, 14, and 5, respectively. The corresponding values for the whole data of the database are 50, 129, 48, 8, 60, and 60, respectively.
The score of citations per document for published Proceeding Articles, Journal Articles, Chapters, Proceedingss, Monographs, and Books by American Institute of Aeronautics and Astronautics (AIAA) are 2.551, 12.864, 0.447, 0.448, 22.611, and 7.681, respectively. The corresponding values for the whole data of the database are 2.540, 11.521, 1.016, 0.199, 9.566, and 8.593, respectively.
The highest number of annually published Proceeding Articles, Journal Articles, Chapters, Proceedingss, Monographs, and Books by American Institute of Aeronautics and Astronautics (AIAA) are 6012, 1474, 185, 35, 14, and 13, respectively. The corresponding year of maximum publication for Proceeding Articles, Journal Articles, Chapters, Proceedingss, Monographs, and Books are 2010, 2020, 2010, 2014, 2015, and 2013, respectively.
The highest number of annual received citations by Proceeding Articles, Journal Articles, Chapters, Proceedingss, Monographs, and Books published in American Institute of Aeronautics and Astronautics (AIAA) are 18921, 22413, 58, 45, 646, and 130, respectively. The corresponding years of maximum received citations for Proceeding Articles, Journal Articles, Chapters, Proceedingss, Monographs, and Books are 2010, 2010, 2015, 2012, 2012, and 2010, respectively.
The highest values of citations per number of document for Proceeding Articles, Journal Articles, Chapters, Proceedingss, Monographs, and Books published in American Institute of Aeronautics and Astronautics (AIAA) are 3.15, 19.14, 0.43, 1.96, 46.14, and 26.00, respectively. The corresponding years of maximum values of citations per document for Proceeding Articles, Journal Articles, Chapters, Proceedingss, Monographs, and Books are 2010, 2010, 2012, 2012, 2012, and 2010, respectively.
Impact Metrics
Various metrics and indicators are used to evaluate the impact and quality of publishers and journals. Here, h-index, g-index, and i-index are selected as impact evaluation metrics of the publisher American Institute of Aeronautics and Astronautics (AIAA).
H-index
H-index indicates the number of articles published by a journal/publisher, h, that have been cited at least h times. h5-index and h10-index are the h-index for papers of a publishers/journals published in the last 5 and 10 years, respectively. h-index, h10-index, and h5-index of the documents published by American Institute of Aeronautics and Astronautics (AIAA), are 254, 80, and 41, respectively. The corresponding values for the whole data of the database are 3269, 1489, and 795, respectively.
Metric | American Institute of Aeronautics and Astronautics (AIAA) | All Publishers |
---|---|---|
h-index | 254 | 3269 |
h10-index | 80 | 1489 |
h5-index | 41 | 795 |
G-index
The g-index indicator is the first g papers of a publisher/journal (sorted by the highest to the lowest number of citations) that have cumulatively received at least g^2 citations. Again, g5-index and g10-index are the g-index for papers of a publishers/journals published in the last 5 and 10 years, respectively. G-index, g10-index, and g5-index of the documents published by American Institute of Aeronautics and Astronautics (AIAA) are 28, 14, and 9, respectively. The corresponding values for the whole data of the database are 131, 80, and 55, respectively.
Metric | American Institute of Aeronautics and Astronautics (AIAA) | All Publishers |
---|---|---|
g-index | 28 | 131 |
g10-index | 14 | 80 |
g5-index | 9 | 55 |
I-n index
I-n index shows the number of publications of a publisher/journal with at least n citations. Read another post here for more detailed information on different research impact metrics. It is to be noted that, i10-index, i25-index, i50-index, i100-index, i250-index, i500-index, i1000-index, i2500-index, i5000-index, and i10000-index of the documents published by American Institute of Aeronautics and Astronautics (AIAA), are 35122, 12312, 4488, 1399, 260, 62, 16, 3, 1, and 0, respectively. The corresponding values for the whole data of the database are 21796896, 10617845, 4822066, 1785083, 390499, 114230, 31648, 5505, 1423, and 355, respectively.
Metric | American Institute of Aeronautics and Astronautics (AIAA) | All Publishers |
---|---|---|
i10-index | 35122 | 21796896 |
i25-index | 12312 | 10617845 |
i50-index | 4488 | 4822066 |
i100-index | 1399 | 1785083 |
i250-index | 260 | 390499 |
i500-index | 62 | 114230 |
i1000-index | 16 | 31648 |
i2500-index | 3 | 5505 |
i5000-index | 1 | 1423 |
i10000-index | 0 | 355 |
Top Journals
This section provides the basic bibliometrics data of the American Institute of Aeronautics and Astronautics (AIAA) top journals, including the number of published documents, total citations, and citations per document. Share of documents and citations of each journal among all published documents by American Institute of Aeronautics and Astronautics (AIAA) is also presented here. In the following tag cloud chart, top journals are displayed based on the largest number of published documents.
The Top 5 journals of American Institute of Aeronautics and Astronautics (AIAA) based on the number of published documents are AIAA Journal, Journal of Aircraft, Journal of Spacecraft and Rockets, Journal of Guidance Control and Dynamics, and Journal of Propulsion and Power. The numbers of documents published so far by these top 5 journals are 26776, 10617, 9816, 7810, and 5565, respectively. These numbers are equal to 9.724%, 3.855%, 3.565%, 2.836%, and 2.021% of the total documents published by American Institute of Aeronautics and Astronautics (AIAA) so far, respectively.
Concerning the number of received citations, the top 5 journals of American Institute of Aeronautics and Astronautics (AIAA) are AIAA Journal, Journal of Guidance Control and Dynamics, Journal of Aircraft, Journal of Propulsion and Power, and Journal of Spacecraft and Rockets. The total number of citations received so far by these top 5 journals are 26776, 7810, 10617, 5565, and 9816, respectively. These numbers are equal to 1.791%, 0.522%, 0.710%, 0.372%, and 0.657% of the total citations received by American Institute of Aeronautics and Astronautics (AIAA) publications so far, respectively.
Regarding the number of citations received per document, the top 5 journals of American Institute of Aeronautics and Astronautics (AIAA) are Journal of Guidance Control and Dynamics, Journal of Guidance and Control, AIAA Journal, Journal of Propulsion and Power, and Journal of Thermophysics and Heat Transfer. The numbers of citations received per published document so far by these top 5 journals are 20.074, 16.833, 16.981, 15.169, and 11.048, respectively.
Journal Title | Documents | Documents Share | Citations | Citations Share | Citations/Documents | Active Years |
---|---|---|---|---|---|---|
AIAA Journal | 26776 | 0.0972 | 450731 | 0.3015 | 16.8334 | 1963-2020 |
Journal of Aircraft | 10617 | 0.0386 | 117294 | 0.0785 | 11.0478 | 1964-2020 |
Journal of Spacecraft and Rockets | 9816 | 0.0356 | 77232 | 0.0517 | 7.8680 | 1964-2020 |
Journal of Guidance Control and Dynamics | 7810 | 0.0284 | 156781 | 0.1049 | 20.0744 | 1978-2020 |
Journal of Propulsion and Power | 5565 | 0.0202 | 84415 | 0.0565 | 15.1689 | 1985-2020 |
Journal of the Aeronautical Sciences (Institute of the Aeronautical Sciences) | 4718 | 0.0171 | 27951 | 0.0187 | 5.9243 | 1934-1957 |
Journal of Thermophysics and Heat Transfer | 3626 | 0.0132 | 41334 | 0.0277 | 11.3993 | 1987-2020 |
Journal of the Aerospace Sciences | 1955 | 0.0071 | 11916 | 0.0080 | 6.0951 | 1958-1962 |
ARS Journal | 1412 | 0.0051 | 5329 | 0.0036 | 3.7741 | 1959-1962 |
Journal of Jet Propulsion | 1361 | 0.0049 | 4348 | 0.0029 | 3.1947 | 1954-1958 |
Journal of Energy | 593 | 0.0022 | 4584 | 0.0031 | 7.7302 | 1977-1983 |
Journal of the American Rocket Society | 577 | 0.0021 | 951 | 0.0006 | 1.6482 | 1945-1953 |
Journal of Hydronautics | 561 | 0.0020 | 2241 | 0.0015 | 3.9947 | 1967-2012 |
Journal of Aerospace Information Systems | 509 | 0.0018 | 1386 | 0.0009 | 2.7230 | 2013-2020 |
Journal of Guidance and Control | 415 | 0.0015 | 7047 | 0.0047 | 16.9807 | 1978-1981 |
Astronautics | 373 | 0.0014 | 49 | 0.0000 | 0.1314 | 1932-1944 |
Air Traffic Control Quarterly | 363 | 0.0013 | 2240 | 0.0015 | 6.1708 | 1993-2015 |
Journal of Aerospace Computing Information and Communication | 310 | 0.0011 | 2992 | 0.0020 | 9.6516 | 2004-2012 |
Bulletin of the American Interplanetary Society | 189 | 0.0007 | 5 | 0.0000 | 0.0265 | 1930-1932 |
Journal of Air Transportation | 108 | 0.0004 | 140 | 0.0001 | 1.2963 | 2016-2020 |
Top Keywords
The Most used keywords are of particular importance for reviewing a publisher. This section provides detailed information about basic bibliometrics data of top used keywords in American Institute of Aeronautics and Astronautics (AIAA). The metrics used here are the number of documents, citations and citations per document. Share of documents and citations of each keyword among whole published documents is also presented here. In the following tag cloud chart, top keywords are displayed based on the largest number of published documents.
According to the number of published documents, the top 10 keywords of the publisher American Institute of Aeronautics and Astronautics (AIAA) are boundary layer, three dimensional, wind tunnel, heat transfer, navier stokes, high speed, numerical simulation, experimental investigation, and control, and finite element, respectively. The number of published documents in which the mentioned 10 keywords are used are, 5390, 3330, 2931, 2830, 2123, 2024, 1963, 1841, 1727, and 1703, respectively.
Based on the number of received citations, the top 10 keywords of the publisher American Institute of Aeronautics and Astronautics (AIAA) are boundary layer, three dimensional, navier stokes, heat transfer, and control, large eddy, two dimensional, finite element, eddy simulation, and wind tunnel, respectively. The number of citations received by the documents in which the mentioned 10 keywords are used are, 5390, 3330, 2123, 2830, 1727, 1285, 1579, 1703, 1142, and 2931, respectively.
Concerning the score of received citations per document, the top 10 keywords of the publisher American Institute of Aeronautics and Astronautics (AIAA) are navier stokes equations, stokes equations, turbulent flow, flow past, low reynolds number, low reynolds, boundary layer transition, layer transition, eddy simulation, and navier stokes, respectively. The score of citations received per document in which the mentioned 10 keywords are used are, 15.734, 15.706, 13.932, 12.544, 11.576, 11.364, 10.846, 10.750, 10.566, and 10.489, respectively.
Keyword | Documents | Documents Share | Citations | Citations Share | Citations/Documents | Active Years | Active Years For All Data |
---|---|---|---|---|---|---|---|
boundary layer | 5390 | 0.1076 | 45429 | 0.0628 | 8.4284 | 1935-2020 | 1915-2020 |
three dimensional | 3330 | 0.0169 | 26433 | 0.0086 | 7.9378 | 1941-2020 | 1500-2020 |
wind tunnel | 2931 | 0.2071 | 11639 | 0.1271 | 3.9710 | 1935-2020 | 1900-2020 |
heat transfer | 2830 | 0.0253 | 18410 | 0.0174 | 6.5053 | 1937-2020 | 1900-2020 |
navier stokes | 2123 | 0.1280 | 22268 | 0.0973 | 10.4889 | 1954-2020 | 1943-2020 |
high speed | 2024 | 0.0204 | 9731 | 0.0148 | 4.8078 | 1934-2020 | 1857-2020 |
numerical simulation | 1963 | 0.0257 | 9951 | 0.0201 | 5.0693 | 1974-2020 | 1962-2020 |
experimental investigation | 1841 | 0.0350 | 9607 | 0.0195 | 5.2184 | 1952-2020 | 1824-2020 |
and control | 1727 | 0.0178 | 13593 | 0.0147 | 7.8709 | 1936-2020 | 1843-2020 |
finite element | 1703 | 0.0110 | 12355 | 0.0097 | 7.2548 | 1963-2020 | 1958-2020 |
two dimensional | 1579 | 0.0100 | 12647 | 0.0048 | 8.0095 | 1939-2020 | 1878-2020 |
control system | 1487 | 0.0214 | 6258 | 0.0280 | 4.2085 | 1935-2020 | 1900-2020 |
flow control | 1460 | 0.1523 | 11006 | 0.1562 | 7.5384 | 1964-2020 | 1896-2020 |
experimental study | 1458 | 0.0118 | 8134 | 0.0080 | 5.5789 | 1948-2020 | 1856-2020 |
boundary layers | 1327 | 0.1640 | 10317 | 0.0817 | 7.7747 | 1935-2020 | 1879-2020 |
reynolds number | 1296 | 0.0633 | 11280 | 0.0346 | 8.7037 | 1934-2020 | 1928-2020 |
large eddy | 1285 | 0.1403 | 12894 | 0.0883 | 10.0342 | 1975-2020 | 1500-2020 |
space station | 1248 | 0.2084 | 1780 | 0.0840 | 1.4263 | 1963-2020 | 1959-2020 |
flight control | 1234 | 0.2523 | 10698 | 0.3561 | 8.6694 | 1960-2020 | 1932-2020 |
flight test | 1227 | 0.4734 | 4754 | 0.6038 | 3.8745 | 1937-2020 | 1922-2020 |
shock wave | 1222 | 0.0647 | 10071 | 0.0611 | 8.2414 | 1947-2020 | 1932-2020 |
turbulent boundary layer | 1186 | 0.2094 | 10420 | 0.1417 | 8.7858 | 1937-2020 | 1932-2020 |
design optimization | 1167 | 0.0884 | 10468 | 0.1016 | 8.9700 | 1964-2020 | 1961-2020 |
numerical study | 1160 | 0.0365 | 8191 | 0.0298 | 7.0612 | 1964-2020 | 1932-2020 |
eddy simulation | 1142 | 0.1528 | 12066 | 0.1049 | 10.5657 | 1979-2020 | 1500-2020 |
space shuttle | 1114 | 0.3824 | 2585 | 0.1932 | 2.3205 | 1970-2020 | 1963-2020 |
leading edge | 1105 | 0.1566 | 8042 | 0.1090 | 7.2778 | 1940-2020 | 1932-2020 |
numerical investigation | 1096 | 0.0530 | 5030 | 0.0345 | 4.5894 | 1965-2020 | 1500-2020 |
gas turbine | 1085 | 0.0439 | 4933 | 0.0416 | 4.5465 | 1948-2020 | 1905-2020 |
propulsion system | 1077 | 0.2890 | 2775 | 0.2886 | 2.5766 | 1943-2020 | 1908-2020 |
solid rocket | 1063 | 0.5198 | 4111 | 0.5416 | 3.8674 | 1962-2020 | 1960-2020 |
launch vehicle | 1025 | 0.4123 | 3536 | 0.5456 | 3.4498 | 1963-2020 | 1962-2020 |
real time | 1021 | 0.0042 | 4383 | 0.0019 | 4.2929 | 1963-2020 | 1900-2020 |
electric propulsion | 986 | 0.3900 | 3848 | 0.4596 | 3.9026 | 1963-2020 | 1888-2020 |
large eddy simulation | 965 | 0.1163 | 10003 | 0.0824 | 10.3658 | 1979-2020 | 1500-2020 |
supersonic flow | 944 | 0.2791 | 7760 | 0.3964 | 8.2203 | 1938-2020 | 1938-2020 |
solid propellant | 911 | 0.4067 | 5518 | 0.4984 | 6.0571 | 1949-2020 | 1941-2020 |
high order | 904 | 0.0390 | 5224 | 0.0195 | 5.7788 | 1963-2020 | 1829-2020 |
wind turbine | 885 | 0.0317 | 3525 | 0.0198 | 3.9831 | 1976-2020 | 1933-2020 |
attitude control | 879 | 0.1813 | 5845 | 0.2297 | 6.6496 | 1959-2020 | 1958-2020 |
rocket motor | 878 | 0.4819 | 2998 | 0.5501 | 3.4146 | 1936-2020 | 1936-2020 |
low reynolds | 869 | 0.1969 | 9875 | 0.1536 | 11.3636 | 1951-2020 | 1930-2020 |
trailing edge | 866 | 0.2548 | 8581 | 0.2758 | 9.9088 | 1955-2020 | 1930-2020 |
fluid dynamics | 852 | 0.0320 | 7174 | 0.0322 | 8.4202 | 1963-2020 | 1929-2020 |
rocket engine | 844 | 0.3877 | 2642 | 0.5046 | 3.1303 | 1942-2020 | 1942-2020 |
jet noise | 820 | 0.5216 | 4872 | 0.3442 | 5.9415 | 1963-2020 | 1953-2020 |
high temperature | 809 | 0.0061 | 3823 | 0.0029 | 4.7256 | 1954-2020 | 1814-2020 |
hypersonic flow | 805 | 0.4340 | 5316 | 0.5641 | 6.6037 | 1950-2020 | 1948-2020 |
high lift | 773 | 0.4766 | 6226 | 0.6271 | 8.0543 | 1940-2020 | 1900-2020 |
angle of attack | 747 | 0.2893 | 4452 | 0.3188 | 5.9598 | 1943-2020 | 1916-2020 |
delta wing | 722 | 0.5205 | 5514 | 0.6773 | 7.6371 | 1953-2020 | 1946-2020 |
conceptual design | 721 | 0.0784 | 2878 | 0.0738 | 3.9917 | 1970-2020 | 1950-2020 |
reduced order | 713 | 0.0843 | 5396 | 0.0853 | 7.5680 | 1971-2020 | 1929-2020 |
flow field | 709 | 0.0367 | 2236 | 0.0156 | 3.1537 | 1945-2020 | 1945-2020 |
flat plate | 677 | 0.0655 | 3624 | 0.0363 | 5.3530 | 1939-2020 | 1735-2020 |
large scale | 673 | 0.0050 | 2897 | 0.0016 | 4.3046 | 1952-2020 | 1500-2020 |
and performance | 660 | 0.0083 | 2765 | 0.0030 | 4.1894 | 1939-2020 | 1666-2020 |
stokes equations | 659 | 0.0613 | 10350 | 0.0624 | 15.7056 | 1954-2020 | 1933-2020 |
navier stokes equations | 657 | 0.0715 | 10337 | 0.0705 | 15.7336 | 1954-2020 | 1943-2020 |
rocket motors | 653 | 0.6114 | 3977 | 0.7469 | 6.0904 | 1936-2020 | 1936-2020 |
hybrid rocket | 646 | 0.5365 | 3925 | 0.6798 | 6.0759 | 1963-2020 | 1963-2020 |
computational fluid dynamics | 644 | 0.0384 | 6367 | 0.0564 | 9.8866 | 1973-2020 | 1970-2020 |
sensitivity analysis | 635 | 0.0218 | 4274 | 0.0167 | 6.7307 | 1968-2020 | 1954-2020 |
optimal control | 629 | 0.0191 | 5716 | 0.0214 | 9.0874 | 1960-2020 | 1900-2020 |
layer interaction | 629 | 0.4506 | 5843 | 0.4445 | 9.2893 | 1957-2020 | 1957-2020 |
system design | 622 | 0.0239 | 2592 | 0.0208 | 4.1672 | 1962-2020 | 1924-2020 |
turbulent flow | 621 | 0.0529 | 8652 | 0.0570 | 13.9324 | 1936-2020 | 1914-2020 |
shape optimization | 617 | 0.1249 | 5755 | 0.1468 | 9.3274 | 1977-2020 | 1974-2020 |
transonic flow | 617 | 0.3593 | 4298 | 0.4383 | 6.9660 | 1946-2020 | 1946-2020 |
boundary layer interaction | 613 | 0.5523 | 5814 | 0.6105 | 9.4845 | 1957-2020 | 1957-2020 |
aspect ratio | 600 | 0.0370 | 3661 | 0.0206 | 6.1017 | 1935-2020 | 1916-2020 |
low cost | 598 | 0.0095 | 1047 | 0.0022 | 1.7508 | 1950-2020 | 1891-2020 |
adaptive control | 592 | 0.0325 | 4891 | 0.0301 | 8.2618 | 1961-2020 | 1954-2020 |
low reynolds number | 589 | 0.1897 | 6818 | 0.1489 | 11.5756 | 1953-2020 | 1934-2020 |
propulsion systems | 585 | 0.2356 | 1942 | 0.2191 | 3.3197 | 1949-2020 | 1932-2020 |
air traffic | 581 | 0.0918 | 2834 | 0.1069 | 4.8778 | 1963-2020 | 1925-2020 |
layer transition | 571 | 0.4117 | 6138 | 0.3761 | 10.7496 | 1939-2020 | 1939-2020 |
high pressure | 570 | 0.0074 | 2191 | 0.0023 | 3.8439 | 1945-2020 | 1815-2020 |
high performance | 568 | 0.0038 | 2018 | 0.0008 | 3.5528 | 1948-2020 | 1922-2020 |
boundary layer transition | 565 | 0.4366 | 6128 | 0.4922 | 10.8460 | 1939-2020 | 1939-2020 |
stability analysis | 556 | 0.0187 | 2772 | 0.0108 | 4.9856 | 1960-2020 | 1943-2020 |
aerodynamic characteristics | 555 | 0.1838 | 2792 | 0.3004 | 5.0306 | 1947-2020 | 1924-2020 |
low speed | 544 | 0.0769 | 2423 | 0.0512 | 4.4540 | 1948-2020 | 1909-2020 |
active control | 537 | 0.0753 | 4354 | 0.0675 | 8.1080 | 1972-2020 | 1936-2020 |
monte carlo | 532 | 0.0062 | 2637 | 0.0023 | 4.9568 | 1963-2020 | 1885-2020 |
numerical analysis | 532 | 0.0149 | 2465 | 0.0129 | 4.6335 | 1962-2020 | 1861-2020 |
two phase | 530 | 0.0124 | 2041 | 0.0042 | 3.8509 | 1957-2020 | 1894-2020 |
heat pipe | 524 | 0.0841 | 2095 | 0.0451 | 3.9981 | 1966-2020 | 1965-2020 |
aircraft design | 523 | 0.3965 | 2166 | 0.4486 | 4.1415 | 1938-2020 | 1918-2020 |
mach number | 510 | 0.0980 | 2580 | 0.0459 | 5.0588 | 1950-2020 | 1941-2020 |
numerical simulations | 510 | 0.0170 | 2915 | 0.0113 | 5.7157 | 1976-2020 | 1500-2020 |
transport aircraft | 506 | 0.3581 | 2723 | 0.4825 | 5.3814 | 1942-2020 | 1935-2020 |
noise reduction | 503 | 0.0452 | 2431 | 0.0369 | 4.8330 | 1947-2020 | 1930-2020 |
flow past | 502 | 0.0894 | 6297 | 0.0960 | 12.5438 | 1950-2020 | 1912-2020 |
control systems | 501 | 0.0139 | 2738 | 0.0097 | 5.4651 | 1943-2020 | 1875-2020 |
reynolds numbers | 498 | 0.1014 | 5127 | 0.0591 | 10.2952 | 1951-2020 | 1929-2020 |
ion thruster | 495 | 0.6387 | 1866 | 0.6947 | 3.7697 | 1966-2020 | 1966-2020 |