Supersonic Engineering: A Symposium Held at the Royal College of Advanced Technology, Salford |
Contents
Safety and Airworthiness Aspects | 29 |
The Noise Problem | 55 |
Power Plants | 62 |
Copyright | |
6 other sections not shown
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Common terms and phrases
acceptable achieved aerodynamic aircraft alloy altitude aluminium angle aspect ratio assumed becomes body cause cent centre characteristics considerable considered costs course cruise curve difficult direct distance drag economic edge effect efficiency engine factor failure flight flow flying frequency fuel function fuselage geometry give given greater heat hence higher important increase installation intake leading length less lift limit load lower Mach Number material maximum means method miles necessary noise nozzle obtained occur operating panel performance position possible present pressure probably problems produce properties range reasonable reduced relatively reliability roll seen shock shown shows skin slender sonic speed stability steel strength stress structure subsonic supersonic aircraft supersonic transport surface take-off temperature thrust transport aircraft trim typical variation wave drag weight wing