Using anisotropic heat flux sensors in aerodynamic experiments
SV Bobashev, NP Mende, PA Popov… - Technical Physics …, 2009 - Springer
We present the results of comparative measurements of the heat flux to a flat plate in a
supersonic flow at a Mach number of M= 6, which were performed using the two following …
supersonic flow at a Mach number of M= 6, which were performed using the two following …
[PDF][PDF] Using Anisotropic Heat Flux Sensors in Aerodynamic Experiments
SV Bobashev, NP Mende, PA Popov… - TECHNICAL …, 2009 - researchgate.net
We present the results of comparative measurements of the heat flux to a flat plate in a
supersonic flow at a Mach number of M= 6, which were performed using the two following …
supersonic flow at a Mach number of M= 6, which were performed using the two following …
Using anisotropic heat flux sensors in aerodynamic experiments
SV Bobashev, NP Mende, PA Popov… - Technical Physics …, 2009 - ui.adsabs.harvard.edu
We present the results of comparative measurements of the heat flux to a flat plate in a
supersonic flow at a Mach number of M= 6, which were performed using the two following …
supersonic flow at a Mach number of M= 6, which were performed using the two following …
Using anisotropic heat flux sensors in aerodynamic experiments.
SV Bobashev, NP Mende, PA Popov… - Technical Physics …, 2009 - search.ebscohost.com
We present the results of comparative measurements of the heat flux to a flat plate in a
supersonic flow at a Mach number of M= 6, which were performed using the two following …
supersonic flow at a Mach number of M= 6, which were performed using the two following …
[引用][C] Using anisotropic heat flux sensors in aerodynamic experiments
SV Bobashev, NP Mende, PA Popov… - Technical Physics …, 2009 - elibrary.ru
Acknowledgments. This study was supported in part by the Russian Foundation for Basic
Research (project nos. 08-08-00414-a and 08-01-91956-NNIO_a) and the Deutsche …
Research (project nos. 08-08-00414-a and 08-01-91956-NNIO_a) and the Deutsche …
Using anisotropic heat flux sensors in aerodynamic experiments.
SV Bobashev, NP Mende, PA Popov… - Technical Physics …, 2009 - search.ebscohost.com
We present the results of comparative measurements of the heat flux to a flat plate in a
supersonic flow at a Mach number of M= 6, which were performed using the two following …
supersonic flow at a Mach number of M= 6, which were performed using the two following …