Page 167 - Aeronautical Engineer Data Book
P. 167

O     < 0.57
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                                             E




         Basic relationships  Some ‘rules of thumb’  Approach speed lies between 1.45 and 1.62 V stall .  W/S = 0.5  V 2 C L  in the ‘approach’ condition.  Approach C L  lies between C Lmax /2.04 and C Lm
      Table 9.3 The ‘first approximations’ methodology










         Estimated parameter   1. Estimate the wing loading   W/S.   2. Check C L  in the cruise.   3. Check gust response at   cruise speed.   4. Estimate size.   5. Estimate take-off wing  loading and T
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