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Portable Network Graphic  |  1997-04-04  |  10KB  |  686x326  |  4-bit (13 colors)

Labels: chat room | hakham | monitor | sky
OCR: CONTROL DIMENSIONS HIGH-LIFT DEVICES CHORD RATIO CONTROL DEFLECTION tlao aileron (up [umop increase in stall angle caused by leading -edge devices (degrees) - elevator or Kruger flaps yield degree increase stall angle stabilator (up down) Slats provide degree increase stall angle CONTROL -EFFECTIVENESS APPROXT IMATION rudder (degrees) wing has NON-FLUSH rivets control surfaces are corrugated and there are control surface gaps roll spoiler (degrees) but wing some has FLUSH control rivets sur1 face smooth gaps control sur faces wing har LUSH rivel smooth control sur faces drag rudder (degrees) pue no control- sur face gap. speedbrake (degrees) flap downl APPROXIMATION smootr 000000 or00 uger angl ONTBOL WinOhaSNONNSS HPPRURIMATION tinn FusH ving

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