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Simulated Landing Approaches of an Unaugmented C-5A Configuration.


AD482810

Publication Date 1966
Personal Author Newell, F. D.; Parrag, M. L. E.; Bull, G.
Page Count 89
Abstract Expected ranges of unaugmented longitudinal and lateral-directional handling qualities of the C-5A class airplane were simulated and evaluated in a variable-stability B-26 for the instrument-landing.
Keywords
  • Jet transport planes
  • Instrument landings
  • Equations of motion
  • Simulation
  • Range(Distance)
  • Stability
  • Ailerons
  • Pitch(Motion)
  • Bomber aircraft
  • Flight simulators
  • Aerodynamic characteristics
  • Yaw
  • Roll
  • Models(Simulations)
  • Aircraft landings
  • Handling
  • B-26 aircraft
  • C-5 aircraft
Source Agency
  • Non Paid Delimited ADS
NTIS Subject Category
  • 51B - Aeronautics
Corporate Authors Cornell Aeronautical Lab Inc Buffalo N Y
Document Type Technical Report
Title Note Final rept.
NTIS Issue Number 197714
Contract Number
  • AF 33(615)-2411
Simulated Landing Approaches of an Unaugmented C-5A Configuration.
Simulated Landing Approaches of an Unaugmented C-5A Configuration.
AD482810

  • Jet transport planes
  • Instrument landings
  • Equations of motion
  • Simulation
  • Range(Distance)
  • Stability
  • Ailerons
  • Pitch(Motion)
  • Bomber aircraft
  • Flight simulators
  • Aerodynamic characteristics
  • Yaw
  • Roll
  • Models(Simulations)
  • Aircraft landings
  • Handling
  • B-26 aircraft
  • C-5 aircraft
  • Non Paid Delimited ADS
  • 51B - Aeronautics
  • AF 33(615)-2411
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