[1] 中国人民解放军总装备部. 军用飞机结构强度规范 第10部分:飞行试验:GJB67.10A-2008 [S]. 北京:总装备部军标出版发行部, 2008:1-5.General Armament Department of PLA. Military air-plane structural strength specification Part10:Flight tests:GJB67.10A-2008 [S]. Beijing:General Arma-ment Department Military Standard Press , 2008:1-5(in Chinese).[2] 中国民用航空局. 中国民用航空规章:CCAR-25-R4 [S]. 北京:中国民1用航空局, 2011:29-58.Civil Aviation Administration of China. Chinese civil aviation regulations: CCAR-25-R4 [S]. Beijing: Civil Aviation Administration of China, 2011:29-58(in Chi-nese).[3] SKOPINSKI T H, AIKEN W S, HUSTON W B. Calibra-tion of Strain-Gage Installations in Aircraft Structures for the Measurement of Flight Loads[R]. NACA Report 1178, 1954.[4] 李俊. 飞机结构载荷测量应变电桥热输出修正方法[J]. 空军工程大学学报(自然科学版),2022,23(1):64-69.LI J. A Thermal Output Correction Method of Strain-Gage Bridge for Load Measurement of Aircraft Struc-ture[J]. Journal of Air Force Engineering University (Natural Science Edition) ,2022,23(1):64-69(in Chi-nese).[5] 李俊, 蒋献. 飞机主动式余度作动舵面铰链力矩飞行测量方法[J]. 空军工程大学学报,2023,24(3):43-49.LI J, JIANG X. A Flight Measurement Method for Hinge Moment of Aircraft Control Surface with Re-dundant Actuation System in Active Mode[J]. Journal of Air Force Engineering University,2023,24(3):43-49(in Chinese).[6] 赵燕, 周占廷, 万小鹏. 剖面内加载对飞行测量载荷的影响[J]. 机械强度,2017,39(5):1061-1065.ZHAO Y, ZHOU Z T,WANG X P. The Effection of Loading Inside Strain-gage Station on Flight Load Measurement[J]. Journal of Mechanical Strength, 2017, 39(5):1061-1065(in Chinese).[7] 赵燕, 周占廷. 某中央翼盒对飞行载荷实测的影响[J]. 航空学报,2016,37(12):3713-3720.ZHAO Y, ZHOU Z T. Effect of Central Wing on Root Flight Load Measurement of certain airfoil[J]. Acta Aeronautica et Astronautica Sinica, 2016,37(12):3713-3720(in Chinese).[8] 张海涛, 余建虎, 李志蕊, 等. T型尾翼布局的尾翼载荷测量技术[J]. 航空学报,2019,40(3):122074.ZHANG H T, YU J H, LI Z R, et al. Measurement Technology for Vertical Fin load of T-shape empen-nage layout[J]. Acta Aeronautica et Astronautica Sinica, 2019,40(3):122074(in Chinese).[9] JECKINS J M, DEANGELIS V M. A Summary of Nu-merous Atrain-Gage Load Calibrations on Aircaft Wings and Tails in a Technology Format[R]. NASA Technical Memorandum 4804. 1997.[10] LOKOS W A, STAUF R. Strain-Gage Loads Calibra-tion Parametric study[R]. NASA/TM-2004-212853. 2004.[11] LOKOS W A, OLNEY C D, CHEN T, et al. Strain Gage Loads Calibration Testing of the Active Aeroelastic Wing F/A-18Aircraft, NASA/TM-2002-210726, 2002.[12] 中国飞行试验研究院. 飞机结构飞行试验指南[M]. 北京:航空工业出版社, 2022: 29-37.Chinese Flight Test Establishment. Aircraft Structural Flight Test Guide[M]. Beijing: Aviation Industry Press, 2022:29-37(in Chinese).[13] 郭正旺, 周友明. 结构完整性试飞-飞机载荷与强度试飞[M]. 北京:航空工业出版社,2018: 18-51.GUO Z W, ZHOU Y M. Flight Test of Structural Integri-ty- Flight Test of Aircraft Load and strength[M]. Beijing: Aviation Industry Press,2018:18-51(in Chinese).[14] CHRISTIAN R, KAI R B. Dynamic flight load meas-urements with MEMS pressure sensors[J]. CEAS Aero-nautical Journal, (2021) 12:737-753.[15] 王志瑾, 姚卫星. 飞机结构设计[M]. 北京: 国防工业出版社,2007:43-102.WANG Z J, YAO W X. Aircraft Structure Design. Bei-jing: National Defense Industry Press, 2007: 43-102(in Chinese).[16] 曹奇凯, 王鄢, 姚念奎等. 先进舰载战斗机强度设计技术发展与实践[J]. 航空学报,2021,v.42(8):525793CAO Q K, WANG Y, YAO N K,Development and Application of Strength Design Technology of Ad-vanced Carrier-based Aircraft[J]. Acta Aeronautica et Astronautica Sinica,2021,v.42(8):525793(in Chinese).[17] 曹景涛, 高尚. 液压多点协调加载技术在机翼载荷校准试验中的应用[J]. 航空科学技术,2015, 26(5):71-75.CAO J T, GAO S. Application of Hydraulic Multipoint Coordinate Loading Technology in Load Calibation Test of Airfoil[J]. Aeronautical Science & Technolo-gy,2015,26(5):71-75(in Chinese).[18] 何发东. 基于多点协调加载试验的机翼飞行载荷模型研究[J]. 机械科学与技术,2015,34(11):1800-1804HE F D. Aircraft Wing Flight Load Model Based on Multiple-point Coordinated Loading Calibration Test[J]. Mechanical Science and Technology for Aerospace Engineering, 2015,34(11):1800-1804(in Chinese).[19] 何发东, 吴波, 李志蕊. 飞机载荷校准试验区域加载技术[J]. 北京航空航天大学学报, 2023,49(10):2867-2872.HE F D, WU B, LI Z R. Zone Loading Technology for Aircraft Load Calibration Test[J]. Journal of Beijing University of Aeronautics and Astronautics, 2023,49(10) :2867-2872(in Chinese). [20] 王黎明, 陈颖, 杨楠. 应用回归分析(第二版)[M]. 上海:复旦大学出版社, 2018: 146-160.WANG L M, CHENG Y, YNAG N. Applied Regression Analysis (Second Edition) [M]. Shanghai: Fudan Uni-versity Press. 2018: 146-160(in Chinese). |