Characteristics of pulse detonation engine versus ramjet characteristics
- 作者: Egoryan A.J.1, Kraiko A.N.1, P’yankov K.S.1, Tishin A.P.2
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隶属关系:
- Central Institute of Aviation Motors by P.I. Baranov
- TESIS Ltd.
- 期: 卷 23, 编号 2 (2016)
- 页面: 297-300
- 栏目: Brief Communications
- URL: https://journals.rcsi.science/1531-8699/article/view/216424
- DOI: https://doi.org/10.1134/S0869864316020177
- ID: 216424
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详细
We discuss the method of comparing pulse detonation engines (PDE) and engines with combustion in subsonic flow (ramjet) by means of their specific impulse used by the “Center of Pulse-Detonation Combustion” (CPDC). We demonstrate that the method used by CPDC to calculate the performance of PDE overstates the value of specific impulse relative to its actual value by a factor of at least two. In contrast, the values of specific impulse for ramjet are understated. As a result, the specific impulse of PDE significantly exceeds that of ramjet or is close to it. We investigate these misleading conclusions, and demonstrate their complete failure.
作者简介
A. Egoryan
Central Institute of Aviation Motors by P.I. Baranov
Email: akraiko@ciam.ru
俄罗斯联邦, Moscow
A. Kraiko
Central Institute of Aviation Motors by P.I. Baranov
编辑信件的主要联系方式.
Email: akraiko@ciam.ru
俄罗斯联邦, Moscow
K. P’yankov
Central Institute of Aviation Motors by P.I. Baranov
Email: akraiko@ciam.ru
俄罗斯联邦, Moscow
A. Tishin
TESIS Ltd.
Email: akraiko@ciam.ru
俄罗斯联邦, Moscow
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