NDLI: Effect of advanced technology and fuel efficient engine on a supersonic-cruise executive jet with a small cabin

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Effect of advanced technology and fuel efficient engine on a supersonic-cruise executive jet with a small cabin

Content Provider	NASA Technical Reports Server (NTRS)
Author	Swanson, E. E. Lovell, W. A. Robins, A. W. Beissner Jr., F. L.
Copyright Year	1983
Description	An analytical study of a supersonic-cruise, executive, jet aircraft indicated the effects of using advanced technology. The twin-engine, arrow-wing vehicle was configured with a cabin of minimum practical size to hold one pilot, eight passengers, and their baggage. The primary differences between this configuration that of a previous report were the reduction in cabin size and the use of engines that are more fuel-efficient. Both conceptual vehicles are capable of forming the same mission. The current vehicle has a range of 3,350 nautical miles at Mach 2.3 cruise and 2,700 nautical miles at Mach 0.9. The concept description includes configuration definition, aerodynamic and propulsion-system characteristics, and mass properties. Performance analyses are documented for intercontinental and transcontinental flight profiles. In the latter case, a reduction in sonic-boom overpressure from 1.3 to 1.0 pounds per square foot was achieved by varying the flight profile slightly from that for optimum performance.
File Size	1129192
Page Count	59
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19830025605
Archival Resource Key	ark:/13960/t8bg7hm1b
Language	English
Publisher Date	1983-08-01
Access Restriction	Open
Subject Keyword	Aircraft Design, Testing And Performance Passenger Aircraft Civil Aviation Aerodynamic Configurations Supersonic Cruise Aircraft Research Aircraft Compartments Fuel Consumption Jet Engines 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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