Reducing the Sonic Boom Level by Heating the Oncoming Airflow


Cite item

Full Text

Open Access Open Access
Restricted Access Access granted
Restricted Access Subscription Access

Abstract

We present the results of calculations of the level of sonic boom in the presence of local heating of the airflow in front of a slender body during its supersonic flight in thermal wake behind the heated regions. The Mach number of a cold oncoming airflow was M = 2. Calculations were performed using a combined method of “phantom bodies.” It is established that sequential local heating of the oncoming airflow in two regions in front of the flying body can reduce the sonic boom level by more than 30% as compared to that in the cold airflow.

About the authors

A. V. Potapkin

Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch,
Russian Academy of Sciences

Author for correspondence.
Email: potapkin@itam.nsc.ru
Russian Federation, Novosibirsk

D. Yu. Moskvichev

Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch,
Russian Academy of Sciences

Email: potapkin@itam.nsc.ru
Russian Federation, Novosibirsk


Copyright (c) 2019 Pleiades Publishing, Ltd.

This website uses cookies

You consent to our cookies if you continue to use our website.

About Cookies