High auxiliary air flow requirements of high speed aircraft place increased emphasis on design of efficient outlets through which air is returned to outside stream; use of small outlets to establish desired pressure fields in certain areas also finds application in boundary layer and aircraft control systems.
Preliminary investigation of aerodynamic characteristics of small inclined air outlets at transonic mach numbers
NACA -- Tech Note
1955
21 pages
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.