An F-15 supersonic fighter aircraft is in a rapid climb. At the instant it passes through a standard altitude of25,000 , its time rate of change of altitude is 500 ft/s, which by definition is the rate-of-climb, discussed in Ch. 6. Corresponding to this rate-of-climb at 25,000 ft is a time rate of change of ambient pressure. Calculate this rate of change of pressure in units of pounds per square foot per second.
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