Stall/Spin/Flight Simulation

Details

• Creators:
  Nagati, M. G.
• Corporate Creators:
  Wichita State University
• Corporate Contributors:
  United States. Department of Transportation. Federal Aviation Administration. Technical Center
• Subject/TRT Terms:
  • Aerodynamics
  • Airplanes
  • Design
  • Rotation
  • Stall
• Publication/ Report Number:
  DOT/FAA/CT-88/28
• Resource Type:
  Tech Report
• Geographical Coverage:
  United States
• Edition:
  Final Report
• Contracting Officer:
  Reed, John
• Corporate Publisher:
  United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center
• Abstract:
  This report summarizes the work performed for stall/spin resistant design aids for aircraft. Two major areas were investigated. First, the solution of the non-linear equations of motion with on-line computation of the aerodynamic moments and visual display of the pilot's view and views of the aircraft. This enables evaluation of the simulator and the quality of the solution by pilots and engineers. Second, a method for predicting the aerodynamics of wings near and beyond stall was developed. It serves the purpose of selecting planforms for spin resistant aircraft. This work demonstrates the viability and promise of these approaches against spin.
• Format:
  PDF
• Funding:
  DTFA03-86-C-00041
• Download URL:
  https://rosap.ntl.bts.gov/view/dot/92980/dot_92980_DS1.pdf
• File Type:
  [PDF - 2.13 MB]
• Collection(s):
  FAA William J. Hughes Technical Center for Advanced Aerospace
• Main Document Checksum:
  urn:sha-512:9813187b10311a1154cd5ba63a24cf550d8e897fcdfa0775c9fc5c8894bb226bcf19feebab7818f7aefe49d87160d36992567f98ece27c23ef74d40899223023