THEORETICAL STUDY OF A NUCLEAR JET ENGINE FOR THE PROPULSION OF AIRPLANES

被引：0

作者：

Mitrica, Bogdan ^{[1
]}

Stanciu, Virgil

Petre, Marian ^{[1
]}

Dima, Mihai ^{[1
]}

Badita, Chivuta ^{[1
]}

Precup, Irinel ^{[1
]}

Petre, Carmelia ^{[1
]}

机构：

[1] Univ POLITEHN Bucuresti, Fac Ingn Aerospatiala, Bucharest, Romania

来源：

UNIVERSITY POLITEHNICA OF BUCHAREST SCIENTIFIC BULLETIN-SERIES A-APPLIED MATHEMATICS AND PHYSICS | 2011年 / 73卷 / 04期

关键词：

nuclear reactor; jet engine; propulsion; airplane;

D O I：

暂无

中图分类号：

O29 [应用数学];

学科分类号：

070104 ;

摘要：

Investigation of the possibility to use a nuclear reactor for the propulsion of airplanes could be performed considering two possible solutions: the direct cycle (the fluid pass through the reactors core) and the indirect cycle (the fluid pass through a heat exchanger). We report about a complete theoretical study which has been performed for the indirect cycles. The cycles, the characteristics and the performances of nuclear jet engine have been calculated. For the nuclear reactor, a homogenous type using UO(2) as fuel, BeO as neutron moderator and B(4)C as the material for the control rods, has been considerate.

引用

页码：139 / 152

页数：14

共 50 条

[41] Measurement System of a Magnetic Suspension System for a Jet Engine Rotor [J].

Kurnyta-Mazurek, Paulina ;

Kurnyta, Artur ;

Henzel, Maciej .

SENSORS, 2020, 20 (03)

[42] Derivation of Rytov variance for jet engine-induced turbulence [J].

Oktay, Semih ;

Bayraktar, Mert ;

Tabaru, Timucin Emre ;

Chatzinotas, Symeon .

PHYSICA SCRIPTA, 2024, 99 (02)

[43] A Novel Communication Protocol for Jet Engine Control and Simulation Platform [J].

Sun, Yongxia ;

Wang, Xi ;

Wang, Lei .

2011 INTERNATIONAL CONFERENCE ON ELECTRONICS, COMMUNICATIONS AND CONTROL (ICECC), 2011, :3506-3509

[44] Design of intelligent diagnosis system based on CBR for jet engine [J].

Xu, B ;

Li, XS ;

Yu, JS .

FIFTH INTERNATIONAL SYMPOSIUM ON INSTRUMENTATION AND CONTROL TECHNOLOGY, 2003, 5253 :1006-1009

[45] Concept of wireless measurement system of UAV jet engine rotor [J].

Kurnyta-Mazurek, Paulina ;

Kurnyta, Artur ;

Henzel, Maciej .

2019 IEEE 6TH INTERNATIONAL WORKSHOP ON METROLOGY FOR AEROSPACE (METROAEROSPACE), 2019, :539-543

[46] Investigation of jet engine intake distortions caused by crosswind conditions [J].

Harjes, Lennart ;

Bode, Christoph ;

Grubert, Jonas ;

Frantzheld, Philip ;

Koch, Patrick ;

Friedrichs, Jens .

JOURNAL OF THE GLOBAL POWER AND PROPULSION SOCIETY, 2020, 4

[47] On the design and structural analysis of jet engine fan blade structures [J].

Amoo, Leye M. .

PROGRESS IN AEROSPACE SCIENCES, 2013, 60 :1-11

[48] Droplet size and spray dispersion characteristics of an impingement-jet type jet engine fuel injector [J].

Tamura, Takahiro ;

Araki, Mikiya ;

Yamada, Hideshi ;

Shiga, Seiichi ;

Hayashi, Shigeru ;

Obokata, Tomio .

Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B, 2008, 74 (10) :2213-2220

[49] An Analytic Study on Mathematical Modeling of Area-Pressure Relation of Jet Engine Convergent-Divergent Nozzles [J].

Wu, Hom-Yu ;

Liao, Kuo-Chien ;

Wen, Hung-Ta .

JOURNAL OF AERONAUTICS ASTRONAUTICS AND AVIATION, 2023, 55 (02) :277-287

[50] Propagation of hyperbolic sinusoidal Gaussian beam in jet engine induced turbulence [J].

Mert Bayraktar ;

Buket Akın ;

Mehmet Berke Işık .

Optical and Quantum Electronics, 2022, 54

← 1 2 3 4 5 →