之路。多学科精细设计方法和多学科设计优化技
ance on fan noise and aerodynamic performance [ R ].
术的大规模应用是提高大型客机安全性 /经济性 /AIAA2200522875 ,2005.
[ 18 ] Horne W, James K, Arledge J , et al. Measurements of 舒适性 /环保性的重要手段和技术实现途径。26 %2scale 777 airframe noise in the NASA ames 402by 80
fort wind tunnel[R]. AIAA2200522810 ,2005.
The future of commercial avia2 tion,buildingonourlegacy[R]. AIAA2200322552 ,2003.
[2] AWIATOR. AWIATOR2Project Overview [ EB/ OL ] ht2 tp :/ / www.awiator. net/project_overview. html
[3] Krumbein A. Automatic transition prediction and applica2 tion to 3D high2lift configurations[R]. AIAA2200623164 , 2006.
[4] Eliasson P. CFD improvements for high lift flows in the european project euroLIFT[R]. AIAA2200323795 ,2003.
[5] CERFACS. Annual Report[EB/OL]. (200727218). ht2 tp://www.cerfacs.fr/cfd/ REPORT20203/ cfd0221007. ht2 ml.
[6] Mc Donnell Douglas Corporation. Evaluation of laminar flow control systems concepts for subsonic commercial transport aircraft[R]. NASA CR2159251 , 1983.
[7] Graaff A D. Participation of EREA in the european union’ saeronautical technology programmes[R]. AIAA220012 5203 ,2001.
[8] Zenkert D. KTH Research Project Database2Advanced lowcostaircraftstructuresALCAS[EB/OL]. http://re2 searchprojects.kth.se/index.php/kb_1/io_9503/ .
[9] Hoffman D J , Bielawski W J. Environmental exposure effectson composite for commercial aircraft[R]. NASA CR2187478 ,1991.
[ 10 ] Wilfert G. Kriegl B , Scheugenpflug H. Clean -validation of a high efficient low nox core , a GTF high speed turbine and an integration of a recuperator in an environmental friendly engine concept[R]. AIAA2200524195 ,2005.
[ 11 ] Ventresca C, Quaglieri R. Analysis process for afford2 abilityand the relationship cost[R]. AIAA2200221767 , 2002.
[ 12 ] Donald J , Sutkus Jr , Baughcum S L. Scheduled Civil air2 craftemissioninventoriesfor1999: databasedevelopment
and analysis[R]. NASA CR220012211216 ,2001.
[ 13 ] Perez2Davis M. Nanotechnology[EB/OL]. (200221127) . http://www. grc. nasa. gov/WWW/AERO/base/zero. ht m
[ 14 ] Loyselle P L. Zero CO2 Emissions technologies project [EB/ OL ]. (200021021) http :/ / www. aeronautics. nasa. gov/ vsp/zeroemissions. htm
[ 15 ] BaughcumSL, TritzTG, HendersonSC,etal. Sched2 uled civil aircraft emission inventories for 1992 : database development and analysis[R]. NASA CR24700 ,1992.
[ 16 ] Randy W , Anderson B E , Connors V S , et al. NASA’s atmospheric effects of aviation project[R]. NASA TM2 20012210829 ,2001.
[ 17 ] Hughes C , Woodward R , Podboy G. Effect of tip clear2
[ 19 ] Elkoby R. Full2scale propulsion airframe aeroacoustics In2 vestigation[R]. AIAA2200522807 , 2005.
[ 20 ] Huysseune J. EU2Flysafe overview[EB/OL]. http:// www. eu2flysafe. org/ EU2Flysafe2Public/ Project/ Over2 view. html
[ 21 ] Luxhoj J , Jalil M , Jones S. A risk2based decision support tool for evaluating aviation technology integration in the national airspace system[R]. AIAA2200326740 ,2003.
[ 22 ] DryerJ. Grants_gov2Find Grant Opportunities2Opport uni2 ty Synopsis[EB/OL]. http://www. grants. gov/search/ search.do? mode=VIEW&oppId=9745.
[ 23 ] NASA. NASA2NASA Dryden Fact Sheet2Intelligent Flight Control System[2007210227]. http://www.nasa. gov/centers/dryden/news/ Factsheets/ FS20762DFRC. ht2 ml.
[ 24 ] Kroo I. Innovations in aeronautics 2004 AIAA dryden lec2 ture[R]. AIAA2200420001 ,2004.
[ 25 ] Bushnell D M. Potential impacts of advanced aerodynamic technologyon air transportation systemproductivity[R]. NASA TM2109154 ,1994.
[ 26 ] Gem F , Ko A , Grossman B , et al. Transport weight re2 duction through MDO: the strut2braced wing transonic transport[R]. AIAA2200524667 ,2005.
[ 27 ] Gundlach J F , Tetrault P A , Gern F. Multidisciplinary design optimization of a strut2Braced wing transonic trans2 port[R]. AIAA2200020402 ,2000.
[28 ] Bagwill T R , Selberg B P. Aerodynamic investigation of twist and cant angles for joined wing transport aircraft
[R]. AIAA29720037 ,1997.
[ 29 ] Dr Nangia R , Dr Palmer M E , Dr Tilmann C. Planform variation effects in unconventional high aspect ratio joined2 wing aircraft incorporating laminar flow[R]. AIAA220052 243 ,2005.
[ 30 ] Liebeck R H , Page M A , Rawdon B K. Blended2wing2
body subsonic commercial transport[R] . AIAA29820438 , 1998.
[ 31 ] Liebeck R H. Design of the blended2wing2body subsonic transport[R]. AIAA2200220002 ,2002.
[ 32 ] Kroo I. Aerodynamic concepts for future aircraft [ R ]. AlAA29923524 ,1999.
[ 33 ] Kroo I. Nonplanar wing concepts for increased aircraft ef2 ficiency[ C] ∥VKI Iecture Series on Innovative Configura2 tions and Advanced Concepts for Future Civil Aircraft. 2005.
[ 34 ] Joner B A , Schneider J J. Evaluation of advanced airship concepts[R]. AIAA 752930 ,1975. 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址:航空学报08大飞机专刊(26)