Spa001dV`˜BV`˜BBOOKMOBI À$@ Ì 4?P is corrected TSFC based on gross thrust _ w f F n ffiffiffiffiffi y T p is corrected TSFC based on net thrust _ w air ffiffiffiffiffi y T p d T is corrected airflow ð 2 16 Þ For the inflight case (namely, V 1 > 0), these total properties, y T and d T, replace the static properties, y and d, respectively, on the axes in Fig 212 Actual data for the J69 engine used in the T37B aircraftÿß T" ` ã J j ã T x " á S ß _ T iPR T NP þP Ji ß í d $ \ÿ *{ÿ P viÿ ¢YP =cl SW ÿ T f ã äPR } S d ÿ Ñn ã J Y æã vb z\ã) Ñf{e ã Ý/ þebß W_ éPSl ã T PjWRã P J TS_Pl T PjWRã Multiple Domination In Graphs Liao Chung Shou 02 Vs 'fÞ t[