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              [html]<thead><tr><td></td><td>TABLE OF</td></tr><tr><td></td><td>Table</td></tr><tr><td>Turbajet operasing limitations... Exhaust gas temperatureCompressor stall or surgeFlamequeCompressor inlet air temperatureEngine speedTime limitaxions</td><td>124</td></tr></thead><tbody><tr><td>Thrust sugmentationAfterburnerWater injection</td><td>129</td></tr><tr><td>The gas turbine - propeller combination. Equivalent shaft horsporerated daily equivalents ( intration ) Operating limitutionPrifymace claacetion</td><td>132</td></tr><tr><td>TJ1E RECIPROCATING ENGINE</td><td>135</td></tr><tr><td>Operating characteristics................................................................................................................................................................................</td><td>Operating cycleBrake hypoplaseInterventions of homeletedNorbal combinetionPregnancies and deronationPorliqualitiesForlinessesInterventions of alternationEffect of altitude and superchargingEffect of homelity</td></tr><tr><td>Long limitations.........................................................................................................................................................................................</td><td>144</td></tr><tr><td>AIRCRAFT PROPELLERS</td><td>Operating characteristics. Flow patterns Populsive efficiency Powerplant matching Governing and feathering</td></tr><tr><td>145</td><td>Operating limitations....................................................................................................................................................................................</td></tr><tr><td>148</td><td>ITEMS OF AIRPLANE PERFORMANCE</td></tr><tr><td>STRAIGHT AND LEVEL FLIGHT</td><td>150</td></tr><tr><td>Equilibrium conditionsThrust and power requiredThrust and power availableMaximum and minimum speed</td><td>CLIMB PERFORMANCE</td></tr><tr><td>150</td><td>Steady and translent climb.................................................................................................................................................................................</td></tr><tr><td>150</td><td>Rate of climb, primary control of altitude Propeller and jet aircraft</td></tr></tbody>
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