(H428.54 sec) the aircraft was at 18,000 feet altitude; zero horizontal
range; and 34,400 feet offset.
The true airspeed was maintained at 800
ft/sec,
In both of the above cases, the actual positions of the aircraft
were very close to the intended positions.
Results
Waiter
Thermal
>
emperature rise in the wing flap (0.025 al. skin)
Gust - 35% design limit in wing bending
Overpressure ae”
<
»
e
Barley
Thermal = negligible
Gust - 60% design limit in side fuselage bending
a
Overpressure ==
se
oy NVI
300/031d09
Mm
aN
~ 48
COeIr none