Electronic Resource
Springer
Communications in mathematical physics
83 (1982), S. 243-260
ISSN:
1432-0916
Source:
Springer Online Journal Archives 1860-2000
Topics:
Mathematics
,
Physics
Notes:
Abstract We study transonic flows along a nozzle based on a one-dimensional model. It is shown that flows along the expanding portion of the nozzle are stable. On the other hand, flows with standing shock waves along a contracting duct are dynamically unstable. This was conjectured by the author based on the study of noninteracting wave patterns. The author had shown earlier that supersonic and subsonic flows along a duct with various cross sections are stable. Basic to our analysis are estimates showing that shock waves tend to decelerate along an expanding duct and accelerate along a contracting duct.
Type of Medium:
Electronic Resource
URL:
http://dx.doi.org/10.1007/BF01976043
| Library |
Location |
Call Number |
Volume/Issue/Year |
Availability |
