VISCOUS COMPRESSIBLE LAMINAR FLOW IN SLENDER AXISYMMETRIC CHANNELS WITH ADIABATIC WALLS

被引:1
作者
ADAMS, JC
WILLIAMS, JC
机构
[1] Dept. of Mechanical and Aerospace Eng., North Carolina State University, Raleigh, N.C.
来源
APPLIED SCIENTIFIC RESEARCH | 1969年 / 21卷 / 02期
关键词
D O I
10.1007/BF00411601
中图分类号
O414.1 [热力学];
学科分类号
摘要
A study is made of the flow of a viscous, compressible, heat conducting, and perfect gas in slender axisymmetric channels under the adiabatic wall condition. Solutions to the equations of motion for such a gas are obtained using the method of similar solutions. This approach reduces the equations of motion to a pair of coupled nonlinear ordinary differential equations which have relatively simple closed form solutions. It is found that solutions of this type are only possible in channels with divergent walls and a favorable pressure gradient. In the present investigation it is found that the velocity profiles are insensitive to moderate variations in the Prandtl number and γ, the ratio of specific heats. The temperature profiles, total temperature profiles, and Mach number profiles are however very sensitive to changes in Prandtl number and ratio of specific heats. For a Prandtl number less than unity there is an accumulation of total energy near the channel centerline and a deficit of total energy near the channel walls. The recovery factor is found to be equal to the Prandtl number. © 1969 Martinus Nijhoff.
引用
收藏
页码:113 / &
相关论文
共 10 条
[1]  
ABBOTT DE, 1960, MD6 STANF U DEP MECH
[2]  
AMES WF, 1965, NONLINEAR PARTIAL DI
[3]  
CHAN YY, 1965, CR284 NASA
[4]  
HANSEN AG, 1964, SIMILARITY ANALYSIS
[5]  
Liepmann H. W., 1957, ELEMENTS GASDYNAMICS
[6]  
RASMUSSEN ML, 1964, SUDAER186 STANF U DE
[7]  
Shapiro A.H., 1953, DYNAMICS THERMODYNAM
[8]  
VANDRIEST ER, 1952, NACA2597 TN
[9]   VISCOUS COMPRESIBLE AND INCOMPRESSIBLE FLOW IN SLENDER CHANNELS [J].
WILLIAMS, JC .
AIAA JOURNAL, 1963, 1 (01) :186-195
[10]   AXISYMMETRIC VISCOUS FLOW PAST VERY SLENDER BODIES OF REVOLUTION [J].
YASUHARA, M .
JOURNAL OF THE AEROSPACE SCIENCES, 1962, 29 (06) :667-&