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Fig. 8.61    Departure and spin suscephbility criteria 43
734          PERFORMANCE, STABILITY, DYNAMlCS, AND CONTROL
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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.                                                     ┃
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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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