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CS-VLA 369 Special conditions for rear lift truss
Available versions for ERULES-1963177438-8062
ED Decision 2003/18/RM
found in: CS-VLA Amdt 1 - Very Light Aeroplanes (Mar 2009)
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CS-VLA Amdt 1 - Ve... (Mar 2009)
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CS-VLA 369 Special conditions for rear lift truss ED Decision 2003/18/RM (a) If a rear lift truss is used, it must be designed for conditions of reversed airflow at a design speed of -  V in m/s M/S = Wing loading (kg/m2) M in kg S in m2 g in m/s2 (b) Either aerodynamic data for the particular wing section used, or a value of CL equaling -0.8 with a chordwise distribution that is triangular between a peak at the trailing edge and zero at the leading edge, must be used.