Russian Aeronautics
ISSN 1068-7998 (Print)
ISSN 1934-7901 (Online)
Menu
Archives
Home
About the Journal
Editorial Team
Editorial Policies
Author Guidelines
About the Journal
Issues
Search
Current
Retracted articles
Archives
Contact
All Journals
User
Username
Password
Remember me
Forgot password?
Register
Notifications
View
Subscribe
Search
Search
Search Scope
All
Authors
Title
Abstract
Index terms
Full Text
Browse
By Issue
By Author
By Title
By Sections
Other Journals
Subscription
Login to verify subscription
Keywords
aircraft
blade
combustion chamber
composite materials
finite element method
gas turbine engine
heat transfer
helicopter
main rotor
mathematical model
mathematical modeling
measurement
numerical modeling
optimization
rocket engine
rotor
spacecraft
stress-strain state
system
unmanned aerial vehicle
wind tunnel
×
User
Username
Password
Remember me
Forgot password?
Register
Notifications
View
Subscribe
Search
Search
Search Scope
All
Authors
Title
Abstract
Index terms
Full Text
Browse
By Issue
By Author
By Title
By Sections
Other Journals
Subscription
Login to verify subscription
Keywords
aircraft
blade
combustion chamber
composite materials
finite element method
gas turbine engine
heat transfer
helicopter
main rotor
mathematical model
mathematical modeling
measurement
numerical modeling
optimization
rocket engine
rotor
spacecraft
stress-strain state
system
unmanned aerial vehicle
wind tunnel
Home
>
Search
>
Author Details
Author Details
Demin, A. V.
Issue
Section
Title
File
Vol 60, No 1 (2017)
Aircraft and Rocket Engine Design and Development
Difference schemes in computations for chemically non-equilibrium processes in the rocket engine nozzles
TOP
