Hartmann–Sprenger effect and its application on aircraft

Authors

  • Viktor Ivanovich Kuznetsov Omsk State Technical University, Omsk, Russia
  • Aleksandra Yur’yevna Shander Omsk State Technical University, Omsk, Russia

DOI:

https://doi.org/10.25206/2588-0373-2019-3-2-150-155

Keywords:

Hartmann–Sprenger effect, viscosity, kinetic energy, aircraft, anti-icing system

Abstract

The question of the effect of viscosity on the occurrence of a stagnation temperature in a dead-end cavity above the deceleration temperature of the incident gas flow the so-called Hartmann–Sprenger effect is considered. It is shown that the Hartmann–Sprenger effect can be used to create the design of the anti-icing system of the aircraft.

Downloads

Download data is not yet available.

Author Biographies

Viktor Ivanovich Kuznetsov, Omsk State Technical University, Omsk, Russia

Doctor of Technical Sciences, Professor of Aviation and Rocketry (AVIRS) Department.

Aleksandra Yur’yevna Shander, Omsk State Technical University, Omsk, Russia

Assistant of AVIRS Department.

Downloads


Abstract views: 16

Published

2019-06-25

How to Cite

Kuznetsov В. И., & Shander А. Ю. (2019). Hartmann–Sprenger effect and its application on aircraft. Omsk Scientific Bulletin. Series «Aviation-Rocket and Power Engineering», 3(2), 150–155. https://doi.org/10.25206/2588-0373-2019-3-2-150-155

Issue

Vol. 3 No. 2 (2019)

Section

Aviation and rocket-space engineering

License

Non-exclusive rights to the article are transferred to the journal in full accordance with the Creative Commons License BY-NC-SA 4.0 «Attribution-NonCommercial-ShareAlike 4.0 Worldwide License (CC BY-NC-SA 4.0»)

Creative Commons License