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              [html]<thead><tr><td>00 – 80T – 80 CONTENTS</td><td>Pspe 238</td></tr></thead><tbody><tr><td>Supersonic engine inlets..................................................................................................................................................................................</td><td>Males, experience</td></tr><tr><td>Supersonic configurations</td><td>240</td></tr><tr><td>AERODYNAMIC HEATING</td><td>242</td></tr><tr><td>Rum temperature rise......................................................................................................................................................................................</td><td>242242</td></tr><tr><td>CHAPTER 4. STABILITY AND CONTROL</td><td>DEFINITIONS</td></tr><tr><td>STATIC STABILITY.........................................................................................................................................................................................</td><td>243245247</td></tr><tr><td>AIRPLANE REFERENCE AXES ·.................................................................</td><td>249</td></tr><tr><td>LONGITUDINAL STABILITY AND CONTROL</td><td>STATIC LONGITUDINAL STABILITY</td></tr><tr><td>250</td><td>General coosiderations. Contribution of the component surfaces................................................................................................................................................</td></tr><tr><td>250253</td><td>Power - of sublisyPower - of sublishPower effectsControl force substant - infection - increased substancesControl force substant - increased - inter - increased - inter - increased - inter - increased - inter - inter - increased - inter - i</td></tr><tr><td>259259264268270</td><td>LONGITUDINAL CONTROL</td></tr><tr><td>275</td><td>Maneuvering control requirementTakeoff control requirement. Landing control requirement.</td></tr><tr><td>275275277</td><td>LONGTTUDINAL DYNAMIC STABILITY</td></tr><tr><td>279</td><td>Phospoid. Short period mosqions</td></tr><tr><td>27.281</td><td>MODERN CONTROL SYSTEMS. Coaventional Boosted Power operated</td></tr><tr><td>281</td><td>DIRECTIONAL STABILITY AND CONTROL</td></tr><tr><td>DIRECTIONAL STABILITY</td><td>284</td></tr><tr><td>Definitions</td><td>284</td></tr><tr><td>Contribution of the sirplase components. Vertical tailVingFastfuge and saccliesPower effects</td><td>285</td></tr><tr><td>Critical conditions</td><td>290</td></tr><tr><td>DIRECTIONAL CONTROL</td><td>290</td></tr><tr><td>Directional control requirements. Adverse yaw</td><td>291291</td></tr><tr><td>xii</td></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr></tbody>
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