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