국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	N+3 Aircraft Concept Designs and Trade Studies : Volume 2;; Appendices-Design Methodologies for Aerodynamics, Structures, Weight, and Thermodynamic Cycles
저자	Greitzer, E. M.;; Bonnefoy, P. A.;; delaRosaBlanco, E.;; Dorbian, C. S.;; Drela, M.;; Hall, D. K.;; Hansman, R. J.;; Hileman, J. I.;; Liebeck, R. H.;; Lovegren, J.;; Mody, P.;; Pertuze, J. A.;; Sato, S.;; Spakovszky, Z. S.;; Tan, C. S.;; Hollman, J. S.;; Duda, J. E.;; Fitzgerald, N.;; Houghton, J.;; Kerrebrock, J. L.;; Kiwada, G. F.;; Kordonowy, D.;; Parrish, J. C.;; Tylko, J.;; Wen, E. A.
Keyword	AERODYNAMIC DRAG;; AERODYNAMICS;; FUSELAGES;; JET PROPULSION;; SUBSONIC AIRCRAFT;; THERMODYNAMIC CYCLES
URL	http://hdl.handle.net/2060/20100042398
보고서번호	NASA/CR-2010-216794/VOL2
발행년도	2010
출처	NTRS (NASA Technical Report Server)
ABSTRACT	Appendices A to F present the theory behind the TASOPT methodology and code. Appendix A describes the bulk of the formulation, while Appendices B to F develop the major sub-models for the engine, fuselage drag, BLI accounting, etc.