NDLI: Fixed base simulator study of an externally blown flap stol transport airplane during approach and landing

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Fixed base simulator study of an externally blown flap stol transport airplane during approach and landing

Content Provider	NASA Technical Reports Server (NTRS)
Author	Carter, C. R. Patton Jr., J. M. Deal, P. L. Nguyen, L. T. Champine, R. A. Grantham, W. D.
Copyright Year	1972
Description	A fixed-base simulator study was conducted to determine the flight characteristics of a representative STOL transport having a high wing and equipped with an external-flow jet flap in combination with four high-bypass-ratio fan-jet engines during the approach and landing. Real-time digital simulation techniques were used. The computer was programed with equations of motion for six degrees of freedom and the aerodynamic inputs were based on measured wind-tunnel data. A visual display of a STOL airport was provided for simulation of the flare and touchdown characteristics. The primary piloting task was an instrument approach to a breakout at a 200-ft ceiling with a visual landing.
File Size	4129047
Page Count	100
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19720025380
Archival Resource Key	ark:/13960/t8hf2m353
Language	English
Publisher Date	1972-10-01
Access Restriction	Open
Subject Keyword	Aircraft Aircraft Landing Transport Aircraft Flight Simulators Aircraft Performance Short Takeoff Aircraft Aerodynamic Characteristics Aircraft Control Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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