Characteristics of Combustion-Driven CO2 Gasdynamic Laser. (II). Effect of Expansion Length of Supersonic Nozzle.

2000 ◽  
Vol 48 (559) ◽  
pp. 257-264
Author(s):  
Tadaharu WATANUKI ◽  
Eiji OGURA ◽  
Yasuhiro MIZOBUCHI ◽  
Satoru MOMO ◽  
Hirotoshi KUBOT
1988 ◽  
Vol 36 (419) ◽  
pp. 550-557
Author(s):  
Tadaharu WATANUKI ◽  
Eiji OGURA ◽  
Yasuhiro MIZOBUCHI ◽  
Shigeru SATO ◽  
Hirotoshi KUBOTA

1977 ◽  
Vol 1 (2) ◽  
pp. 73-74 ◽  
Author(s):  
A. Demetriades
Keyword(s):  

1977 ◽  
Vol 11 (1) ◽  
pp. 95-100
Author(s):  
V. A. Vinogradov ◽  
M. D. Petrov

2014 ◽  
Vol 590 ◽  
pp. 546-550
Author(s):  
Zhi Qiang Fan ◽  
Hai Bo Yang ◽  
Fei Zhao ◽  
Rong Zhu ◽  
Dong Bai Sun

The practical requirements of the project the nozzle entrance temperature is high, the gas specific heat ratio varies greatly, so it must consider the specific heat ratio change impact on two-dimensional nozzle contour design. Divided into consideration specific heat ratio change and not consider two kinds of scheme design of 1.4Ma nozzle profile and build the model using the arc line method, numerical simulation is carried out through the CFD software Fluent, analysis of two kinds of design scheme comparison. The results show that, in the supersonic nozzle at low Maher numbers, two schemes of nozzle design profile similarity, parameters change little flow tube, export the Maher number and the flow quality can meet the design requirements, proof of specific heat ratio has little effect on the design results in the design of the nozzle under the condition of low Maher number.


1979 ◽  
Vol 15 (6) ◽  
pp. 743-753 ◽  
Author(s):  
M. G. Ktalkherman ◽  
V. M. Mal'kov ◽  
A. Yu. Shevyrin ◽  
G. Yu. Sheitel'man

2022 ◽  
Author(s):  
Manoj Prabakar Sargunaraj ◽  
Andres Torres ◽  
Jose Garduna ◽  
Marcel Otto ◽  
Jayanta S. Kapat ◽  
...  

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