NDLI: Application of nasa-arc delayed flap approach procedures to boeing 727 airplane

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Application of nasa-arc delayed flap approach procedures to boeing 727 airplane

Content Provider	NASA Technical Reports Server (NTRS)
Author	Allison, R. L.
Copyright Year	1977
Description	The results of an engineering and piloted simulator study to adapt a NASA developed-approach energy management system (AEMS) concept to the B727 are presented. The AEMS concept was developed and flight tested on a CV-990. The purpose of the AEMS is to reduce approach time, fuel, and noise by providing computer-driven cockpit displays to assist the pilot in flying optimized delayed flap approach (DFA) procedures. Development of the DFA flight profiles, the AEMS airborne digital computer algorithm, and associated cockpit displays were studied. Study ground rules and pertinent aerodynamic and noise trend data used in developing the flight profiles are presented. Approach time, fuel, and noise for the DFA are compared to several other types of procedures.
File Size	3948070
Page Count	103
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19770012117
Archival Resource Key	ark:/13960/t48q0t50s
Language	English
Publisher Date	1977-02-01
Access Restriction	Open
Subject Keyword	Aircraft Design, Testing And Performance Nasa Programs Noise Reduction Boeing 727 Aircraft Flaps Control Surfaces Energy Policy Approach Control Computer Aided Design Flight Simulation Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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