Calculation of heat transfer on the catalytically active surface of high-speed aircraft
The scientific paper analyzes the influence of the catalytically active surface on the intensity of heat and mass transfer in a chemically active boundary layer. Some features of the mechanism of heat and mass transfer under conditions of heterogeneous catalysis are indicated. Heat transfer analysis...
Main Authors: | Petr V. NIKITIN, Olga V. TUSHAVINA, Anna A. SHKURATENKO |
---|---|
Format: | Article |
Language: | English |
Published: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2019-08-01
|
Series: | INCAS Bulletin |
Subjects: |
Similar Items
-
Boundary layer of the dissociated gas flow over a porous wall under the conditions of equilibrium dissociation
by: Obrović Branko, et al.
Published: (2005-01-01) -
Thermal control of spacecraft star sensor attitude control system based on the solution of a coupled thermoelasticity problem
by: S. V. Tsaplin, et al.
Published: (2016-07-01) -
Acoustic Analysis of Spacecraft Cavities using the Boundary Element Method
by: Marshall, Peter Johannes
Published: (2018) -
Conductive and convective heat transfer with radiant heat flux boundary conditions
by: Sikka, Satish
Published: (2011) -
Thermal protection of aircraft units using film cooling with regard to unsteady heat conductivity
by: Lev N. RABINSKIY, et al.
Published: (2019-08-01)