Zobrazeno 1 - 10
of 27
pro vyhledávání: '"Michael Todorov"'
Publikováno v:
13TH INTERNATIONAL SCIENTIFIC CONFERENCE ON AERONAUTICS, AUTOMOTIVE AND RAILWAY ENGINEERING AND TECHNOLOGIES (BulTrans-2021).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::eb7db219228e3a7a9fe586bf3a380707
https://doi.org/10.1063/5.0105571
https://doi.org/10.1063/5.0105571
Publikováno v:
17TH INTERNATIONAL CONFERENCE ON CONCENTRATOR PHOTOVOLTAIC SYSTEMS (CPV-17).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d8bd8dc2336b65624793e102098bb659
https://doi.org/10.1063/5.0092112
https://doi.org/10.1063/5.0092112
Publikováno v:
13TH INTERNATIONAL SCIENTIFIC CONFERENCE ON AERONAUTICS, AUTOMOTIVE AND RAILWAY ENGINEERING AND TECHNOLOGIES (BulTrans-2021).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8d8651c44b85b3bc4ff20dda816da823
https://doi.org/10.1063/5.0106920
https://doi.org/10.1063/5.0106920
Publikováno v:
2020 New Trends in Civil Aviation (NTCA).
This paper presents the results of an experimental study of the aerodynamic performance of a helicopter rotor for UAV applications in steady hover at Reynolds numbers below 50 000 by means of particles image velocimetry (PIV). Results are shown for a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2d878d14b38b2b5af16a5e46c6925461
https://doi.org/10.23919/ntca50409.2020.9291224
https://doi.org/10.23919/ntca50409.2020.9291224
Autor:
Todinov, Michael Todorov
Publikováno v:
International Journal of Risk Assessment and Management; 2023, Vol. 26 Issue: 1 p1-16, 16p
Publikováno v:
Review of the Air Force Academy. 15:27-36
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8e45577c5eabee5896d9124b082a9f5c
https://doi.org/10.19062/1842-9238.2017.15.3.3
https://doi.org/10.19062/1842-9238.2017.15.3.3
Publikováno v:
SCIENTIFIC RESEARCH AND EDUCATION IN THE AIR FORCE. 19:153-164
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5601ccc1baf304e26a1ad9a115c59b4b
https://doi.org/10.19062/2247-3173.2017.19.1.16
https://doi.org/10.19062/2247-3173.2017.19.1.16
Publikováno v:
2019 International Conference on Military Technologies (ICMT).
In this paper are presented the results of an experimental study on the performance of a helicopter rotor model in hover during transient operation. The aim of this study is to quantitatively evaluate the variations of the aerodynamic forces, resulti
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6da3db36ed6475b16add69573dfb3311
https://doi.org/10.1109/miltechs.2019.8870035
https://doi.org/10.1109/miltechs.2019.8870035
Publikováno v:
IOP Conference Series: Materials Science and Engineering. 1002:012001
Due to the motion of tip and root vortices of helicopter rotor blades and the inevitable blade-vortex interactions in multi-blade rotors, the profile drag of all individual blades is increased, when compared to the absence of any blade-vortex interac
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::66c90e5c0b6bf55104e5f1075cda09a7
https://doi.org/10.1088/1757-899x/1002/1/012001
https://doi.org/10.1088/1757-899x/1002/1/012001
Autor:
Michael Todorov, Cvetelina Velkova
Publikováno v:
Review of the Air Force Academy. 13:39-44
The purpose of the study is to assess what the influence of the distance of the gap is between the wing and slotted flap on the aerodynamic characteristics of ultra-light aircraft wing when the flap is retracted. It has been elected numerical approac
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1ae317edda03fd06295a16c6796950bb
https://doi.org/10.19062/1842-9238.2015.13.3.6
https://doi.org/10.19062/1842-9238.2015.13.3.6