The calculated performance of airplanes equipped with supercharging engines (1921)
NASA Technical Reports Server (NTRS) · leaf 33
owing 7it' as a function of u for various altitudes. Such a set of curves for the Liberty engine with turbine-driven supercharging compressor on the Le Pere plane is shown on figure 15. The method of plotting these curves will be discussed in the next article. For the present we_ will concern… … ~SO 60 70 30 SO /OO f/O /20 /30 /40 /50 /60 /70. f/ff. /4. Sp eecf of Advance - M7/esper t-fr. obvious that ht must-equal 7<t'. Hence the reduced value of the maximum horizontal flight speed at afay altitude is the value of uior the point where the curve, y=Jitr(u)> for the given altitude crosses…
NASA Technical Reports Server (NTRS)
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