국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	A Method for Designing Blended Wing-Body Configurations for Low Wave Drag
저자	Raymond L. Barger
Keyword	Supersonic aircraft design; Blended wing-body; Low-drag design
URL	http://techreports.larc.nasa.gov/ltrs/PDF/tp3261.pdf
보고서번호	NASA TP-3261
발행년도	1992
출처	NASA Langley Research Center
ABSTRACT	A procedure for tailoring a blended wing-body configuration to reduce its computed wave drag is described. The method utilizes an iterative algorithm within the framework of first-order linear theory. Four computed examples are included. In each case, the zero-lift wave drag was reduced without an increase in drag due to lift.