Cite
A method for estimating the change in pressure of a local supersonic flow on the aerodynamic control surface profile when a transonic flatter occurs
MLA
Safronov, O. V., et al. “A Method for Estimating the Change in Pressure of a Local Supersonic Flow on the Aerodynamic Control Surface Profile When a Transonic Flatter Occurs.” Science and Defence, Oct. 2019. EBSCOhost, widgets.ebscohost.com/prod/customlink/proxify/proxify.php?count=1&encode=0&proxy=&find_1=&replace_1=&target=https://search.ebscohost.com/login.aspx?direct=true&site=eds-live&scope=site&db=edsair&AN=edsair.scientific.p..d2b56bc43f46f6d62b9f6756ece81ba8&authtype=sso&custid=ns315887.
APA
Safronov, O. V., Semon, B. Y., & Nedilko, O. M. (2019). A method for estimating the change in pressure of a local supersonic flow on the aerodynamic control surface profile when a transonic flatter occurs. Science and Defence.
Chicago
Safronov, O. V., B. Y. Semon, and O. M. Nedilko. 2019. “A Method for Estimating the Change in Pressure of a Local Supersonic Flow on the Aerodynamic Control Surface Profile When a Transonic Flatter Occurs.” Science and Defence, October. http://widgets.ebscohost.com/prod/customlink/proxify/proxify.php?count=1&encode=0&proxy=&find_1=&replace_1=&target=https://search.ebscohost.com/login.aspx?direct=true&site=eds-live&scope=site&db=edsair&AN=edsair.scientific.p..d2b56bc43f46f6d62b9f6756ece81ba8&authtype=sso&custid=ns315887.