text: The variation of thrust output with engine 
  speed is a factor of great importance in the 
  operation of the turbojet engine. By reason- 
  ing that static pressure changes depend on the 
  square of the flow velocity, the changer of 
  pressure throughout the turbojet engine would 
  
  <html>
          <head> <meta charset="UTF-8">
          <style>
          table, th, td {
              border: 1px solid black;
              font-size: 10px;
          }
          </style> </head>
          <body>
          <table frame="hsides" rules="groups" width="100%%">
              [html]<thead><tr><td>Vt = inlet or flight velocity, fr. per sec. Vf = jet velocity, ft. per see.</td><td>Since an increase in flight speed will increase the magnitude of V1, a constant thruse will be</td></tr></thead><tbody><tr></tr><tr></tr><tr></tr><tr></tr></tbody>
          </table> </body> </html>
  
  116 