Citation: | FU Junquan, SHI Zhiwei, CHEN Jie, ZHOU Mengbei, WU Dawei, PAN Lijun. Departure characteristics of blended-wing-body aircraft[J]. Journal of Experiments in Fluid Mechanics, 2020, 34(6): 32-37. DOI: 10.11729/syltlx20190110 |
[1] |
AMMAR S, LEGROS C, TRÉPANIER J-Y. Conceptual design, performance and stability analysis of a 200 passengers Blended Wing Body aircraft[J]. Aerospace Science and Technology, 2017, 71:325-336. DOI: 10.1016/j.ast.2017.09.037
|
[2] |
ORDOUKHANIAN E, MADNI A M. Blended Wing Body architecting and design:current status and future prospects[J]. Procedia Computer Science, 2014, 28:619-625. DOI: 10.1016/j.procs.2014.03.075
|
[3] |
朱自强, 王晓璐, 吴宗成, 等.民机的一种新型布局形式:翼身融合体飞机[J].航空学报, 2008, 29(1):49-59. DOI: 10.3321/j.issn:1000-6893.2008.01.007
ZHU Z Q, WANG X L, WU Z C, et al. A new type of transport-blended wing body aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2008, 29(1):49-59. DOI: 10.3321/j.issn:1000-6893.2008.01.007
|
[4] |
付军泉, 史志伟, 周梦贝, 等.一种翼身融合飞行器的失速特性研究[J].航空学报, 2020, 41(1):123176. https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB202001005.htm
FU J Q, SHI Z W, ZHOU M B, et al. Stall characteristics research of blended-wing-body aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(1):123176. https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB202001005.htm
|
[5] |
QIN N, VAVALLE A, LE MOIGNE A, et al. Aerodynamic considerations of blended wing body aircraft[J]. Progress in Aerospace Sciences, 2004, 40(6):321-343. DOI: 10.1016/j.paerosci.2004.08.001
|
[6] |
LI P F, ZHANG B Q, CHEN Y C, et al. Aerodynamic design methodology for blended wing body transport[J]. Chinese Journal of Aeronautics, 2012, 25(4):508-516. DOI: 10.1016/S1000-9361(11)60414-7
|
[7] |
LYU Z J, MARTINS J R R A. Aerodynamic design optimization studies of a blended-wing-body aircraft[J]. Journal of Aircraft, 2014, 51(5):1604-1617. DOI: 10.2514/1.C032491
|
[8] |
LARKIN G, COATES G. A design analysis of vertical stabilisers for Blended Wing Body aircraft[J]. Aerospace Science and Technology, 2017, 64:237-252. DOI: 10.1016/j.ast.2017.02.001
|
[9] |
JOHNSTON D E, HOGGE J R. Nonsymmetric flight influence on high-angle-of-attack handling and departure[J]. Journal of Aircraft, 1976, 13(2):112-118. DOI: 10.2514/3.58639
|
[10] |
马军, 宋晋, 刘蓓, 等.立式风洞全视场尾旋姿态测量技术研究[J].实验流体力学, 2016, 30(6):66-70, 104. http://www.syltlx.com/CN/abstract/abstract10982.shtml
MA J, SONG J, LIU B, et al. Design and implementation for full field of view measurement scheme in vertical wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2016, 30(6):66-70, 104. http://www.syltlx.com/CN/abstract/abstract10982.shtml
|
[11] |
杨文, 卜忱, 眭建军.某复杂构型飞机偏航-滚转耦合运动非定常气动力特性实验研究[J].实验流体力学, 2016, 30(3):61-65. http://www.syltlx.com/CN/abstract/abstract10935.shtml
YANG W, BU C, SUI J J. Investigation of the unsteady aerodynamic characteristics of a fighter with complex configuration undergoing yaw-roll coupling oscillation motion[J]. Journal of Experiments in Fluid Mechanics, 2016, 30(3):61-65. http://www.syltlx.com/CN/abstract/abstract10935.shtml
|
[12] |
许光明.飞机失速/偏离问题研究的技术途径[J].气动实验与测量控制, 1990, 4(3):1-6. https://www.cnki.com.cn/Article/CJFDTOTAL-LTLC199003000.htm
XU G M. The technical approaches to investigation of stall/departure problems of aircraft[J]. Aerodynamic experiment and measurement & control, 1990, 4(3):1-6. https://www.cnki.com.cn/Article/CJFDTOTAL-LTLC199003000.htm
|
[13] |
张洪.飞机大迎角飞行稳定性判据分析[J].航空学报, 1988, 9(10):B502-505. https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB198810012.htm
ZHANG H. Flight stability criteria analysis of aircraft at high angles-of-attack[J]. Acta Aeronautica et Astronautica Sinica, 1988, 9(10):B502-505. https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB198810012.htm
|
[14] |
李树有, 王启, 张培田.飞机失速/尾旋特性的预测和试验研究[J].飞行力学, 2000, 18(3):42-45. DOI: 10.3969/j.issn.1002-0853.2000.03.011
LI S Y, WANG Q, ZHANG P T. Prediction and test of aircraft stall/spin characteristics[J]. Flight Dynamics, 2000, 18(3):42-45. DOI: 10.3969/j.issn.1002-0853.2000.03.011
|
[15] |
李永富.用风洞技术预测飞机的失速/尾旋特性[J].航空与航天, 2004(4):12-15, 18.
|
[16] |
耿玺, 史志伟.面向过失速机动的风洞动态试验相似准则探讨[J].实验流体力学, 2011, 25(3):41-45. DOI: 10.3969/j.issn.1672-9897.2011.03.010
GENG X, SHI Z W. Similarity criterion of the wind tunnel test for the post-stall maneuver[J]. Journal of Experiments in Fluid Mechanics, 2011, 25(3):41-45. DOI: 10.3969/j.issn.1672-9897.2011.03.010
|
[17] |
郭林亮, 祝明红, 傅澔, 等.水平风洞中开展飞机尾旋特性研究的理论分析[J].航空学报, 2018, 39(6):79-90. https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201806008.htm
GUO L L, ZHU M H, FU H, et al. Theoretical analysis of research on aircraft spin characteristic in horizontal wind tunnel[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(6):79-90. https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201806008.htm
|
[18] |
LUTZE F H, DURHAM W C, MASON W H. Unified development of lateral-directional departure criteria[J]. Journal of Guidance, Control, and Dynamics, 1996, 19(2):489-493. DOI: 10.2514/3.21644
|
[19] |
MENGALI G, GIULIETTI F. Unified algebraic approach to approximation of lateral-directional modes and departure criteria[J]. Journal of Guidance, Control, and Dynamics, 2004, 27(4):724-728. DOI: 10.2514/1.6606
|
[20] |
Tinger H L. Departure resistance and spin characteristics of the F-15 S/MTD[R]. AIAA-89-0012, 1989.
|
[21] |
ARAUJO-ESTRADA S A, LOWENBERG M H, NEILD S, et al. Evaluation of aircraft model upset behaviour using wind tunnel manoeuvre rig[R]. AIAA 2015-0750, 2015.
|
[22] |
LAWRENCE F, MILLS B. Status update of the AEDC wind tunnel Virtual Flight Testing development program[R]. AIAA 2002-0168, 2002.
|