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┃ I ┃ ┃
┃ I ┃ ┃
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Fig. 8.61 Departure and spin suscephbility criteria 43
734 PERFORMANCE, STABILITY, DYNAMlCS, AND CONTROL
-o
OEPARTUR~
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┃ . \ ┃ A F-i02 r odei Test : z8- ┃
┃ o ┃ V F-106 F~ight Test: 30'-3 ┃
┃ u ┃-o-oo. A o SAAB 37 Flight kst:>35 ┃
┃ . d ┃ ┃
┃ ┃-Jc=Io- ,.:,,.-":3, t=3o* ┃
┣━━━━━━━┳━━━━╋━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━┫
┃'OO",l"::l-O~ ┃-r I ┃(=40,.0-,4:'-Bo. ocC,c - -0-,1s 0.0 d ┃
┃ ┃ c ┃ ┃
┃ ┃ ┃- - o.oo. ┃
┗━━━━━━━┻━━━━┻━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━┛
Fig. 8.62 Application of C,,ODYN and LCDP criteria.43
divergence in yaw followed by a roll reversal. In region C, the aircraft is likely
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