Year 2016, Volume 17 , Issue 5, Pages 936 - 952 2016-12-20

ENERGY AND ENTROPY ANALYSES OF AN EXPERIMENTAL TURBOJET ENGINE FOR TARGET DRONE APPLICATION

Onder Turan [1]


This study investigates energy and entropy analyses of an experimental turbojet engine build in Anadolu University Faculty of Aeronautics and Astronautics Test-Cell Laboratory.  Law of motions and Brayton thermodynamic cycle model are used for this purpose. The processes (that is, compression, combustion, and expansion) are simulated in P-v, T-s and h-s diagrams. Furthermore, the second law of thermodynamics is applied to the cycle model to perform the entropy analysis. A distribution of the wasted and thrust power, the overall (energy-based the first law efficiency), and the specific fuel consumption and specific thrust of the engine were calculated during the analyses as well. The results of the study also show the entropy changing value in engine components due to irreversibilities and inefficiencies. As a conclusion, it is expected that this study is useful to study future design and research work similar aircraft turbojets, auxiliary power units and target drone power systems.

Subjects Engineering
Journal Section Articles
Authors

Author: Onder Turan

Dates

Publication Date : December 20, 2016

Bibtex @ { aubtda279861, journal = {Anadolu University Journal of Science and Technology A - Applied Sciences and Engineering}, issn = {1302-3160}, eissn = {2146-0205}, address = {}, publisher = {Eskisehir Technical University}, year = {2016}, volume = {17}, pages = {936 - 952}, doi = {10.18038/aubtda.279861}, title = {ENERGY AND ENTROPY ANALYSES OF AN EXPERIMENTAL TURBOJET ENGINE FOR TARGET DRONE APPLICATION}, key = {cite}, author = {Turan, Onder} }
APA Turan, O . (2016). ENERGY AND ENTROPY ANALYSES OF AN EXPERIMENTAL TURBOJET ENGINE FOR TARGET DRONE APPLICATION . Anadolu University Journal of Science and Technology A - Applied Sciences and Engineering , 17 (5) , 936-952 . DOI: 10.18038/aubtda.279861
MLA Turan, O . "ENERGY AND ENTROPY ANALYSES OF AN EXPERIMENTAL TURBOJET ENGINE FOR TARGET DRONE APPLICATION" . Anadolu University Journal of Science and Technology A - Applied Sciences and Engineering 17 (2016 ): 936-952 <https://dergipark.org.tr/en/pub/aubtda/issue/26583/279861>
Chicago Turan, O . "ENERGY AND ENTROPY ANALYSES OF AN EXPERIMENTAL TURBOJET ENGINE FOR TARGET DRONE APPLICATION". Anadolu University Journal of Science and Technology A - Applied Sciences and Engineering 17 (2016 ): 936-952
RIS TY - JOUR T1 - ENERGY AND ENTROPY ANALYSES OF AN EXPERIMENTAL TURBOJET ENGINE FOR TARGET DRONE APPLICATION AU - Onder Turan Y1 - 2016 PY - 2016 N1 - doi: 10.18038/aubtda.279861 DO - 10.18038/aubtda.279861 T2 - Anadolu University Journal of Science and Technology A - Applied Sciences and Engineering JF - Journal JO - JOR SP - 936 EP - 952 VL - 17 IS - 5 SN - 1302-3160-2146-0205 M3 - doi: 10.18038/aubtda.279861 UR - https://doi.org/10.18038/aubtda.279861 Y2 - 2020 ER -
EndNote %0 Anadolu Üniversitesi Bilim Ve Teknoloji Dergisi A - Uygulamalı Bilimler ve Mühendislik ENERGY AND ENTROPY ANALYSES OF AN EXPERIMENTAL TURBOJET ENGINE FOR TARGET DRONE APPLICATION %A Onder Turan %T ENERGY AND ENTROPY ANALYSES OF AN EXPERIMENTAL TURBOJET ENGINE FOR TARGET DRONE APPLICATION %D 2016 %J Anadolu University Journal of Science and Technology A - Applied Sciences and Engineering %P 1302-3160-2146-0205 %V 17 %N 5 %R doi: 10.18038/aubtda.279861 %U 10.18038/aubtda.279861
ISNAD Turan, Onder . "ENERGY AND ENTROPY ANALYSES OF AN EXPERIMENTAL TURBOJET ENGINE FOR TARGET DRONE APPLICATION". Anadolu University Journal of Science and Technology A - Applied Sciences and Engineering 17 / 5 (December 2016): 936-952 . https://doi.org/10.18038/aubtda.279861
AMA Turan O . ENERGY AND ENTROPY ANALYSES OF AN EXPERIMENTAL TURBOJET ENGINE FOR TARGET DRONE APPLICATION. AUBTD-A. 2016; 17(5): 936-952.
Vancouver Turan O . ENERGY AND ENTROPY ANALYSES OF AN EXPERIMENTAL TURBOJET ENGINE FOR TARGET DRONE APPLICATION. Anadolu University Journal of Science and Technology A - Applied Sciences and Engineering. 2016; 17(5): 936-952.