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              [html]<thead><tr><td>NAVWEPS 00 – 80T – 80 INDEX</td><td>propeljers</td></tr></thead><tbody><tr><td>Page</td><td>characteristics.........................................................................................................................................................................................</td></tr><tr><td>145</td><td>efficiency</td></tr><tr><td>145</td><td>operaeang limitations....................................................................................................................................................................................</td></tr><tr><td>148</td><td></td></tr><tr><td>efficiency</td><td>106</td></tr><tr><td>principles</td><td>104</td></tr><tr><td>ram temperature rise</td><td>242</td></tr><tr><td>range pcrformance</td><td>158</td></tr><tr><td>of - optimum conditions....................................................................................................................................................................................</td><td>172</td></tr><tr><td>propellet airplance......................................................................................................................................................................................</td><td>turbojet airplanes</td></tr><tr><td>164</td><td>rate of climited reciprocating</td></tr><tr><td>154</td><td>operating characteristics</td></tr><tr><td>135</td><td></td></tr><tr><td>operating limitations.</td><td>144</td></tr><tr><td>Tefusal speed</td><td>392</td></tr><tr><td>Percentage blade stall</td><td>402</td></tr><tr><td>Preversed command region</td><td>353</td></tr><tr><td>Reynolds number</td><td>54</td></tr><tr><td>Parameters</td><td>59</td></tr><tr><td>Separation, airflow</td><td>56</td></tr><tr><td>Construction</td><td>328</td></tr><tr><td>Shock induced separation</td><td>218</td></tr><tr><td>Shock wave formation......................................................................................................................................................................................</td><td>218</td></tr><tr><td>Available</td><td>284</td></tr><tr><td>Slipstream results</td><td>294</td></tr><tr><td>Sonic booms</td><td>396</td></tr><tr><td>Spanwise lift distribution</td><td>74</td></tr><tr><td>Aspecific endurance....... specific fucl consumption</td><td>170</td></tr><tr><td>reciprocating engine..</td><td>141</td></tr><tr><td>Ratio</td><td></td></tr><tr><td>117</td><td>Specific range</td></tr><tr><td>158</td><td>speed, maximum and minimum..................</td></tr><tr><td>150</td><td>spin, spin recovery</td></tr><tr><td>307</td><td>Stability and Control, Chapter IV.................................................................................................................</td></tr><tr><td>243</td><td>directional.</td></tr><tr><td>284</td><td>dynamic</td></tr><tr><td>245</td><td></td></tr><tr><td>helicopter</td><td>319</td></tr><tr><td>latera. l</td><td>294</td></tr><tr><td>longitudinal</td><td>250</td></tr><tr><td>Providers - control - control - control - control - control - control - control - control - control - control - control - control - control - control - control - control - control - control - control - control - control - control - control - contro</td><td>305</td></tr><tr><td>Static</td><td>243</td></tr><tr><td>Stall specds</td><td>35</td></tr><tr></tr><tr></tr></tbody>
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