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OpenAlex Citation Counts

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OpenAlex is a bibliographic catalogue of scientific papers, authors and institutions accessible in open access mode, named after the Library of Alexandria. It's citation coverage is excellent and I hope you will find utility in this listing of citing articles!

If you click the article title, you'll navigate to the article, as listed in CrossRef. If you click the Open Access links, you'll navigate to the "best Open Access location". Clicking the citation count will open this listing for that article. Lastly at the bottom of the page, you'll find basic pagination options.

Requested Article:

Aircraft Gas-Turbine Engine’s Control Based on the Fuel Injection Control
Alexandru-Nicolae Tudosie
InTech eBooks (2011)
Open Access | Times Cited: 26

Showing 1-25 of 26 citing articles:

An investigation into factors determining the metering performance of a fuel control unit in an aero engine
Yuan Yuan, Tianhong Zhang, Zhonglin Lin, et al.
Flow Measurement and Instrumentation (2019) Vol. 71, pp. 101672-101672
Closed Access | Times Cited: 21
Speed control system for a jet-engine with fluid injection into its compressor
Alexandru-Nicolae Tudosie
(2014), pp. 1-6
Closed Access | Times Cited: 8
Aircraft engine with coolant injection into its compressor and flow rate controller as controlled object
Alexandru-Nicolae Tudosie
(2016), pp. 1-6
Closed Access | Times Cited: 8
Aircraft Gas-Turbine Engine with Coolant Injection for Effective Thrust Augmentation as Controlled Object
Alexandru Nicolae Tudosie
InTech eBooks (2018)
Open Access | Times Cited: 7
A mimicking technique of back pressure in the hardware-in-the-loop simulation of a fuel control unit
Yuan Yuan, Zhiwen Zhao, Tianhong Zhang
SIMULATION (2019) Vol. 96, Iss. 4, pp. 375-385
Open Access | Times Cited: 7
Supplementary fuel control system for a jet-engine with fluid injection into its combustor
Alexandru-Nicolae Tudosie
(2014), pp. 1-6
Closed Access | Times Cited: 4
Mathematical model of an indirect action fuel flow controller for aircraft jet engines
Alexandru Nicolae Tudosie
AIP conference proceedings (2017) Vol. 1836, pp. 020063-020063
Open Access | Times Cited: 3
Aircraft dual-shaft jet engine with indirect action fuel flow controller
Alexandru Nicolae Tudosie
AIP conference proceedings (2017) Vol. 1836, pp. 020064-020064
Open Access | Times Cited: 3
Embedded control system for an aircraft two-spool jet engine with coolant injection into the compressor
Alexandru-Nicolae Tudosie
(2018), pp. 67-72
Closed Access | Times Cited: 3
GROUND TEST FACILITY FOR A TURBOSHAFT-TYPE APU TG-16M FOR PASSENGER AIRCRAFT
Alexandru-Nicolae Tudosie
SCIENTIFIC RESEARCH AND EDUCATION IN THE AIR FORCE (2016) Vol. 18, Iss. 1, pp. 85-92
Open Access | Times Cited: 2
Improved super-twisting fuzzy sliding mode control based on fuel regulator
J.-f. Feng D. Qi, Weiwei Liu, Yang Wang, et al.
Research Square (Research Square) (2024)
Open Access
Engine Speed Control Unit for an Aircraft Jet Engine with Coolant Injection into the Combustor
Alexandru-Nicolae Tudosie
(2018), pp. 1-6
Closed Access | Times Cited: 2
Hydro-mechanical fuel flow controller for aircraft jet engines
Alexandru-Nicolae Tudosie
(2017) Vol. 2, pp. 343-348
Closed Access | Times Cited: 1
Aircraft single-jet engine with hydro-mechanical fuel flow controller
Alexandru-Nicolae Tudosie
(2017)
Closed Access | Times Cited: 1
MATHEMATICAL MODEL FOR AN AIRCRAFT TURBOSHAFT-TYPE AUXILIARY POWER UNIT
Alexandru-Nicolae Tudosie
Review of the Air Force Academy/Revista Academiei Forţelor Aeriene "Henri Coandă" (2017) Vol. 15, Iss. 3, pp. 161-170
Open Access | Times Cited: 1
The simulation and analysis of fault diagnosis and isolation for gas turbine control system
Muhammad Shahzad Qamar Asif
(2018)
Closed Access | Times Cited: 1
Injection System for an Aircraft Jet Engine with Coolant Injection into the Combustor
Alexandru-Nicolae Tudosie
(2018), pp. 1-6
Closed Access | Times Cited: 1
Aircraft Single-Jet Engine with Hydro-Mechanical Thrust Augmentation System Based on Coolant Injection into the Compressor
Alexandru-Nicolae Tudosie
(2019), pp. 1-6
Closed Access | Times Cited: 1
Speed Control System for a Low-bypass Turbofan with Coolant Injection into its Compressor
Alexandru-Nicolae Tudosie
(2023), pp. 439-444
Closed Access
AIRCRAFT HYDRO-MECHANICAL NOZZLE VERSUS PNEUMO- HYDRAULIC NOZZLE AS CONTROLLED OBJECTS
Alexandru Nicolae Tudosie
SCIENTIFIC RESEARCH AND EDUCATION IN THE AIR FORCE (2023) Vol. 24, pp. 185-195
Open Access
Flow Measurement: An Inverse Problem Formulation
Jiwei Li, Lingyun Qiu, Zhongjing Wang, et al.
SIAM Journal on Applied Mathematics (2023) Vol. 83, Iss. 4, pp. 1654-1676
Open Access
Aircraft Jet-Engine Exhaust Nozzle with Pneumatic-Hydraulic Control Unit
Alexandru-Nicolae Tudosie
2022 8th International Conference on Control, Decision and Information Technologies (CoDIT) (2023), pp. 945-949
Closed Access
Embedded control system for an aircraft two-spool jet engine with coolant injection into the compressor
Alexandru-Nicolae Tudosie
(2018), pp. 389-394
Closed Access
Embedded Control System for an Aircraft High Bypass Turbofan with Coolant Injection into the Compressor
Alexandru-Nicolae Tudosie
(2022), pp. 192-197
Closed Access
Ідентифікація багаторежимної моделі авіаційних двигунів вертольотів у польотних режимах з використанням модифікованого градієнтного алгоритму навчання радіально-базисних нейронних мереж
С.І. Владов, І.О. Дєрябіна, О.В. Гусарова, et al.
Вісник Херсонського національного технічного університету (2021) Vol. 79, Iss. 4, pp. 52-63
Open Access
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