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기술보고서

기술보고서 게시판 내용
타이틀	Advanced Technology Subsonic Transport Study: N+3 Technologies and Design Concepts
저자	Raymer, Daniel P.;; Wilson, Jack;; Perkins, H. Douglas;; Rizzi, Arthur;; Zhang, Mengmeng;; RamirezPuentes, Alfredo
Keyword	AEROELASTICITY;; AIRLINE OPERATIONS;; BOEING 737 AIRCRAFT;; CANARD CONFIGURATIONS;; COMMERCIAL AIRCRAFT;; DESIGN ANALYSIS;; FUEL CONSUMPTION;; NASA PROGRAMS;; NOISE REDUCTION;; RUDDERS;; SUBSONIC SPEED;; TRANSPORT AIRCRAFT;; WINGS
URL	http://hdl.handle.net/2060/20110023431
보고서번호	NASA/TM-2011-217130
발행년도	2011
출처	NTRS (NASA Technical Report Server)
ABSTRACT	Conceptual Research Corporation, the Science of the Possible, has completed a two-year study of concepts and technologies for future airliners in the 180-passenger class. This NASA-funded contract was primarily focused on the ambitious goal of a 70 percent reduction in fuel consumption versus the market-dominating Boeing 737-800. The study is related to the N+3 contracts awarded in 2008 by NASA s Aeronautics Research Mission Directorate to teams led by Boeing, GE Aviation, MIT, and Northrop Grumman, but with more modest goals and funding. CRC s contract featured a predominant emphasis on propulsion and fuel consumption, but since fuel consumption depends upon air vehicle design as much as on propulsion technology, the study included notional vehicle design, analysis, and parametric studies. Other NASA goals including NOx and noise reduction are of long-standing interest but were not highlighted in this study, other than their inclusion in the propulsion system provided to CRC by NASA. The B-737-800 was used as a benchmark, parametric tool, and design point of departure. It was modeled in the RDS-Professional aircraft design software then subjected to extensive parametric variations of parasitic drag, drag-due-to-lift, specific fuel consumption, and unsized empty weight. These studies indicated that the goal of a 70 percent reduction in fuel consumption could be attained with roughly a 30 percent improvement in all four parameters. The results were then fit to a Response Surface and coded for ease of use in subsequent trade studies. Potential technologies to obtain such savings were identified and discussed. More than 16 advanced concept designs were then prepared, attempting to investigate almost every possible emerging concept for application to this class airliner. A preliminary assessment of these concepts was done based on their total wetted area after design normalization of trimmed maximum lift. This assessment points towards a Tailless Airliner concept which was designed and analyzed in some detail. To make it work, a retracting canard and an all-moving chin rudder were employed, along with the use of the Active Aeroelastic Wing technology. Results indicate that a 60 percent savings in fuel burn may be credibly attained, but this depends upon a lot of technology maturation, concept development, and risk reduction. This should be expected-such a dramatic reduction in fuel consumption is a "game changer" in the world of commercial aviation. It won t be easy.