PERFORMANCE, STABILITY, DYNAMICS, AND CONTROL1(117)

Æعą̂ ×¢Òâ·ÀÆ­ ÍøÆØÌìèµê¸»ÃÀ½ðÊ¢¼Ò¾ÓרӪµê¿ÓÃɹÕÆ­ÆÛÕ©Ïû·ÑÕß

©§    ©§      ©§/   ©§  ©§  ©§    ©§    ©§                                  ©§              ©§    ©§        ©§                      ©§    ©§  ©§    ©§  ©§
©§')  ©§:hec: ©§iry ©§  ©§  ©§    ©§    ©§                                  ©§              ©§    ©§        ©§                      ©§    ©§  ©§    ©§  ©§
©§    ©§      ©§    ©§  ©§  ©§    ©§    ©§       .                          ©§              ©§    ©§        ©§                      ©§    ©§  ©§    ©§  ©§
©§    ©§      ©§    ©§  ©§  ©§    ©§    ©§            J-                    ©§              ©§    ©§        ©§                      ©§    ©§  ©§    ©§  ©§
©§    ©§      ©§    ©§TAN§€TAN AI.E
    (pet rad)
0    .:Z   .4    .6   .8   1.0   .8   .6    .4   .'1   O
                   -l-                                TAN A L9
         TAN ALE                   a
a)
o    .Z   .4   .6   .8
 -/-
         TAN A7E
.6    .4    .'1    0
TAN ,\ LE
          =
     p
Fig. 3.14    Supersonic normal-force-curve slope of wings.l
179
CNa) theory
   (per rad)
3(CNa,) th,ory
2 (pcrrad)
 I
o
  ] .0           .8
b)

"}

180          PERFORMANCE, STABILI-fY, DYNAMICS, AND CONTROL
                                                                                                                         
                                                                                                                         
¡¡
Öйúº½¿ÕÍø www.aero.cn
º½¿Õ·­Òë www.aviation.cn
±¾ÎÄÁ´½ÓµØÖ·£ºPERFORMANCE, STABILITY, DYNAMICS, AND CONTROL1(117)