|Table of Contents|

Scramjet engine nozzle design with variable specific heat(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2010年02期
Page:
43-47
Research Field:
研究与设计
Publishing date:

Info

Title:
Scramjet engine nozzle design with variable specific heat
Author(s):
Wang Yufeng;  Wu BaoYuan;  Wang Dongdong
Xi'an Aerospace Propulsion Institute, Xi'an 710100, China
Keywords:
-
PACS:
V439
DOI:
-
Abstract:
When the gas stagnation temperature increases, the specific heat ratio starts to vary with the temperature. Scramjet engine nozzle inlet temperature is very high and the influence of specific heat variation must be taken into account. This paper describes a method for scramjet engine nozzle design. A comparison between calorically perfect gas and that of thermally perfect gas is given.

References:

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Memo

Memo:
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