국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	Damage Arresting Composites for Shaped Vehicles - Phase II Final Report
저자	Velicki, Alex;; Yovanof, Nicolette;; Baraja, Jaime;; Linton, Kim;; Li, Victor;; Hawley, Arthur;; Thrash, Patrick;; DeCoux, Steve;; Pickell, Robert
Keyword	AERODYNAMIC CONFIGURATIONS;; BLENDED-WING-BODY CONFIGURATIONS;; DAMAGE;; FUSELAGES;; INTERNAL PRESSURE;; PULTRUSION;; RODS;; WINGS
URL	http://hdl.handle.net/2060/20110004279
보고서번호	NASA/CR-2011-216880
발행년도	2011
출처	NTRS (NASA Technical Report Server)
ABSTRACT	This report describes the development of a novel structural concept, Pultruded Rod Stitched Efficient Unitized Structure (PRSEUS), that addresses the demanding fuselage loading requirements for the Hybrid Wing or Blended Wing Body (BWB) airplane configuration. In addition to the analytical studies, a three specimen test program was also completed to assess the concept under axial tension loading, axial compression loading, and internal pressure loading.