[1] |
朱自强,吴宗成,陈迎春等. 民机空气动力学设计先进技术. 上海:上海交通大学出版社,2013
|
[2] |
李广义,张晋平. 国际航空,2011,2:47
|
[3] |
温坤. 国际航空,2011,6:67
|
[4] |
朱自强,鞠胜军,吴宗成. 航空学报,2016,37(7):2065
|
[5] |
Schrauf G. The Aeronautical J.,2005,109(1102):639
|
[6] |
Thibert J J,Reneaux J,Schmitt R V. ONERA activities on drag reduction.ICAS-90-3.6.1,1990
|
[7] |
Liebeck R H. Journal of Aircraft,2004,41(1):10
|
[8] |
Holmes B J,Clifford J,Martin G L et al. Manufacturing tolerances for natural laminar flow airframe surface. SAE paper 850863,1985
|
[9] |
Saric W S,Reed H L,White E B. Annu. Rev. Fluid Mech.,2003,35:413
|
[10] |
Collier F S. An overview of recent subsonic laminar flow control flight experiments. AIAA 93-2987,1993
|
[11] |
Kirchner M E. Laminar flow:challenge and potential. NASACP-2487,part1,1987. 25—44
|
[12] |
Joslin R D. Overview of laminar flow control. NASATP-208705,1998
|
[13] |
Arcara P C,Bartlett D W,Mecullers L A. Analysis for the application of hybrid laminar flow control to a long rang subsonic transport aircraft. SAE Paper 912113,1991
|
[14] |
Wagner R D,Maddalon D V,Fisher D F. Journal of Aircraft,1990,27(3):239
|
[15] |
Maddalon D V. Hybrid laminar flow control flight research.NASATM4331,1991
|
[16] |
Crouch J D. Boundary layer transition prediction for laminar flow control. AIAA 2015-2472,2015
|
[17] |
Bonet J T. Boeing ERA N+2 advanced vehicle concept results.In:50th AIAA aerospace science meeting,Jan.11,2012
|
[18] |
Thomas R H,Burley C L,Olson E D. Hybrid wing body aircraft system noise assessment with propulsion airframe aeroacoustic experiments. AIAA 2010-3913,2010
|
[19] |
张正国. 国际航空,2010,2:56
|
[20] |
Jameson K K,Marshall D D,Ehrmann R et al. CalPoly’s AMELIA 10 foot span hybrid wing body low noise CESTOL aircraft wind tunnel test and experimental results overview. AIAA-2013-0974,2013
|
[21] |
朱自强,吴宗成. 航空学报. 2016,37(2):411
|
[22] |
Zeune C H. An overview of the airforce's speed agile concept demonstration program. AIAA 2013-1097,2013
|
[23] |
Gundlach J F,Naghshineh-Pour A H,Gern F et al. Multidisciplinary design optimization and industry review of a 2010 strut-braced wing transonic transport. VPI-MAD99-06-03,1999
|
[24] |
Gern F,Ko A,Grossman B et al. Transport weight reduction through MDO:The strut-braced wing transonic transport. AIAA 2005-4667,2005
|
[25] |
Nam T,Chakraborty I,Gross J et al. Multidisciplinary design optimization of a truss-braced wing concept. AIAA 2014-2423,2014
|
[26] |
Graham W. Trauss-braced wing shows promise. AW&ST,2015-01-12
|
[27] |
Greitzer E M,Bonnefoy P A,Dela R B et al. N+3 Aircraft Concept Designs and Trade Studies,Final Report,Vol1,Vol2,NASA CR-2010-216794,2010
|
[28] |
Mark D. Development of the D8 Transport Configuration. AIAA2011-3970,2011
|