Stall/Spin/Flight Simulation

Nagati, M. G.

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Stall/Spin/Flight Simulation

1989-09-01
By Nagati, M. G.

File Language:

English

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
Collection(s):

FAA William J. Hughes Technical Center for Advanced Aerospace
Main Document Checksum:

urn:sha-512:9813187b10311a1154cd5ba63a24cf550d8e897fcdfa0775c9fc5c8894bb226bcf19feebab7818f7aefe49d87160d36992567f98ece27c23ef74d40899223023
Download URL:

https://rosap.ntl.bts.gov/view/dot/92980/dot_92980_DS1.pdf
File Type:

[PDF - 2.13 MB ]

File Language:

English

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