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Tests on Thrust Augmenters for Jet Propulsion (1932)
NASA Technical Reports Server (NTRS) · leaf 8
Fig. 3 NACA Technical IToto llo. 431 1.5 With Molot-type augmontor 1.4 1.3 With long throat / (D Venturi only. CD Ch 1.1 -With Vontiiri only. / Cm O ^Thoortical thrust of -/roc jot, … Theoretical thrust from* K-1 K 4 1 i .4 IT tMt^,-,) ^^'^-)^ W^-<^^ .3 " K , Ratio of specific heats for air, , Ilozzle throat area. .2 " Pp , Absolute reservoir pressure. Pa , Absolute atmospheric pressure. .1 20 40 50 80 100 120 140 160 180 200 Reservoir pressure, lb. per sq. in. G-ago Pig^J-re…NASA Technical Reports Server (NTRS)
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