Exploratory tests of aerodynamic characteristics of model of the case of the bearing form

The article is devoted to exploratory tests of the main integrated aerodynamic characteristics of model of the bearing case of the heavy aircraft. In article results of purges of the studied model are given in an air tunnel. The analysis of the received results is carried out. The main conclusions on article are drawn, the main advantages of the case of not round form are noted. On the high bearing properties and high aerodynamic quality recommendations of expediency of ways of further researches are made.