Altitude performance of J35-A-17 turbojet engine in an altitude chamber

Vincent, K. R., Gale, B. M.
naca-rm-e50i15
1951


Simulated flight performance of a J35-A-17 turbo-jet engine in an altitude chamber is presented for range of altitudes from 20,000 to 30,000 feet at flight Mach number of 0.62 and for range of flight Mach numbers from 0.42 to l.22 at altitude of 30,000 feet.

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