SUPERSONIC EXPIRATION OF GAS OUT OF ASYMMETRIC VESSEL OF FINITE WIDTH DURING MAXIMUM EXPENDITURE

摘要

In work is considered steady supersonic expiration of stream of ideal adiabatic compressible gas out of asymmetric vessel with flat parallel walls. Fall of pressure outside of and inside vessel is assumed so large that ensures maximum magnitude of expenditure of gas. As a result of solution of appearing boundary value problem in mixed region of sub and supersonic speeds of flow will succeed to explain how asymmetry of walls of vessel have influence on the angular displacement of a stream from the initial direction of flow.