1
مکانیک::
محل تقاطع پوشش موتور با بال
• cowling the wing-nacelle intersection with fairings which will reduce the pressure gradient after the maximum airfoil thickness
;Flow separation area in the wing-nacelle intersection.
A more successful and less expensive approach was the modification of the wing-nacelle intersection with different fairings.
Modified wing-nacelle intersection with an optimized fairing.
For the real aircraft the exhaust gases of the engine could be blown into the wing-nacelle intersection with a volume flow rate of 30 ls-1.
واژگان شبکه مترجمین ایران