the aircraft was
DELETED
DELETED
Results
Thermal PB.perature rise in the gray test panel in the
wing flap.
Gust - Not availahle at this time.
Barley
DELETED
Thermal . & yyieh "
Gust « s design limit in side fuselage bending.
Overpressure DELETE" |
Special ~ Damage
Waiter
Flap - The paint
S
»
Stabilator - Damage to the gray test panel of the stabilator was
comparable to that received in the flap.
Fuselage ~
DELETED
Poa
COPIED/ DOE
LANL Re
97
.
eat
5