text: THE V-B OR V-g DIAGRAM 
  
  due to the gust condition are higher. This is 
  explained by 
  that essentially the 
  same lift change acts on the lighter mass. 
  The high accelerations and 
  forces 
  magnify the impression of the magnitude of 
  If this same airplane encounters 
  turbulence. 
  the gust condition at higher 
  than ordinary 
  gross weight, the accelerations due to the gust 
  condition are lower, i.e., the same lift change 
  the gteatet mass. Since the pilot 
  acts on 
  primarily senses the degree of turbulence by 
  the resulting accelerations and inertia forces, 
  this effect can produce a very misleading 
  impression. 
  The operating flight strength limitations of 
  an airplane are presented in the form of a 
  V-‘-n or V-g diagram. This chart usually is 
  included in the aircraft flight handbook in the 
  limitations. 
  section dealing with operating 
  A typical V-n diagram is shown in figure 5.3. 
  The V-n diagram presented in figure 5.3 is 
  intended to present the most important general 
  features of such a diagram and does not neces- 
  sarily represent the characteristics of any par- 
  ticular airplane. Each airplane type has its 
  own particular V-n diagram with specific V’s 
  and n’s, 