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Fighter Combat - Tactics and Maneuvering

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APPENDIX 391<br />

Figure A-2. Aircraft Turn Performance<br />

maximized by high G at slow speed. Since the V-n diagram of a fighter<br />

specifies its G capabilities at various speeds, it is possible to determine<br />

turn-rate <strong>and</strong> -radius performance throughout the aircraft's speed range.<br />

Figure A-3 is a depiction of the way typical fighter turn-performance varies<br />

with airspeed.<br />

In the case of turn rate, the rapid rise in G capability as speed increases<br />

above Vs (as shown by the lift boundary in the V-n diagram) leads to<br />

improved instantaneous-turn-rate performance, culminating at Vc. Since<br />

load factor is limited by structural considerations, however, further increases<br />

in airspeed above Vc result in reduced turn rate. Typical fighter<br />

turn-radius performance also is degraded (i.e., RT increases) at speeds above<br />

Vc. Although absolute minimum instantaneous turn radius is usually<br />

found at speeds considerably below Vc, little change can be expected in RT

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