Data show variation in pressure with indicated airspeed and angle of sideslip for both canopy closed and canopy open conditions; effect of admitting cockpit ventilating air; variation of pressure with normal acceleration at constant value of free stream impact pressure; method for predicting pressure in accelerated flight from measurements made in unaccelerated flight.
Flight measurements of internal cockpit pressures in several fighter-type airplanes
Nat Advisory Committee Aeronautics -- Tech Note
1947
9 pages
20 Supp Plates
Report
English
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SOME HIGH SPEED EXPERIENCE WITH FIGHTER TYPE AIRPLANES
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