GBT16638.4-1996空气动力学概念、量和符号第4部分飞行器的空气动力、力矩及其系数和导数.pdf 22页

'ICS49020免费标准下载网(www.freebz.net)v04中华人民共和国国家标准Gs/T16638.4-1996空气动力学概念、量和符号第4部分飞行器的空气动力、力矩及其系数和导数Aerodynamics-Concepts,quantitiesandsymbolsPart4Aerodynamicforces,moments,theircoefficientsandderivativesofaircraft1996一12一13发布1997一06一01实施国家技术监督局发布免费标准下载网(www.freebz.net)无需注册即可下载 免费标准下载网(www.freebz.net)目次前言····················，·······························，························································。····⋯⋯皿1范围···············································································································⋯⋯12引用标准··················。····················，··············································。··················⋯⋯13术语和符号···························································。························。·······。·········⋯⋯13.1空气动力、力矩及其系数·······································································..·..........⋯⋯13.1.1空气动力合力、合力矩························，······················。···························.·.......⋯⋯13.1.2气流坐标轴系的空气动力、力矩及其系数············。································.·..·..·.⋯⋯，·.⋯13.1.3机体坐标轴系的空气动力、力矩及其系数··············································.............⋯⋯33.1.4半机体坐标轴系的空气动力、力矩及其系数···············，·········································⋯⋯33.1.5作用在操纵面上的力、力矩及其系数················，···················································一53.2空气动力导数·························································································..·..·.··一63.2.1空气动力静导数····。·······························。···························...·.········。··.·.⋯⋯，·.⋯63.2.2空气动力动导数·············⋯⋯，’’·······························。····。·‘···············⋯.⋯，·····⋯⋯83.2.3空气动力操纵导数·······················································。··········.···········.·.....·..一n汉语索引(按汉语拼音顺序编排).............................................··...................................14英文索引(按英文字母顺序编排)....................................................................................16标准分享网www.bzfxw.com免费下载免费标准下载网(www.freebz.net)无需注册即可下载 免费标准下载网(www.freebz.net)GB/T16638.4-1996前言本标准参照采用国际标准ISO1151《飞行动力学—概念、量和符号》并与国家标准GB/T14410.2-93《飞行力学概念、量和符号力矩及其系数和导数》相协调。本标准是系列标准《空气动力学概念、量和符号》中的一个，其他标准还有:GB/T16638.1-1996《空气动力学概念、量和符号第1部分空气动力学常用术语》;GB/T16638.2-1996《空气动力学概念、量和符号第2部分坐标轴系和飞行器运动状态量》;GB/T16638.3-1996《空气动力学概念、量和符号第3部分飞行器的几何特性》。本标准由航空工业总公司提出。本标准由航空工业总公司301所归口。本标准由北京航空航天大学、航空工业总公司627所等单位负责起草。本标准主要起草人:冯亚南、范洁川、陈玉、张克军。免费标准下载网(www.freebz.net)无需注册即可下载 免费标准下载网(www.freebz.net)中华人民共和国国家标准空气动力学概念、量和符号第4部分飞行器的空气动力、力矩及其系数和导数GB/"r16638.4-1996Aerodynamics-Concepts,quantitiesandsymbolsPart4Aerodynamicforces,moments.theircoefficientsandderivativesofaircraft范围本标准规定了飞行器的空气动力、力矩及其系数和导数的术语和符号。本标准主要适用于具有固定翼的航空飞行器，其他飞行器可参照使用。本标准将飞行器视为刚体引用标准下列标准所包含的条文，通过在本标准中引用而构成为本标准的条文。本标准出版时.所示版本均为有效。所有标准都会被修订.使用本标准的各方应探讨使用下列标准最新版本的可能性。GB/T16638.2-1996空气动力学概念、量和符号第2部分坐标轴系和飞行器运动状态量33131术语和符号空气动力、力矩及其系数空气动力合力、合力矩编号一术语定义或说明符号一一空气动力合力作用于飞行器或其部件的空气动左」laerodynamicresultantf、)rce力的合力向壁一{一3.1.1.2一一空气动力合力矩合力向量对力矩参考点的力矩，aerodynarnlcresultantrnoment{1.2气流坐标轴系的空气动力、力矩及其系数国家技术监督局1996一12一13批准1997一06一01实施标准分享网www.bzfxw.com免费下载免费标准下载网(www.freebz.net)无需注册即可下载 免费标准下载网(www.freebz.net)GB/T16638.4一1996编号术语"&"’定义或说明符号R戌在气流坐标轴系2。轴负方向3.1.2.1护的分量。气流坐标轴系定义见LGB/T16638.2中2.1.4:/(合，VZS{升力系数3。1.2.2式中p为自由流密度，V为自由流Cl.llftcoefficient速度，5为参考面积，通常取机翼面积或机身最大横截面积R月在气流坐标轴系二。轴负方向3.1。2.3竖力DUldg的分量阻力系数D/(告，V’5!3。1.2.4Cndragcoefficient式中P，V，5的含义同3.122侧力3.1.2.5侧在气流坐标轴系y.轴的分量C或Y。cross一strearnforce侧力系数C/(合、25{3.1.2。6’ccross一streamforcecoefficient式中P，V，5的含义同3.1，22气流轴俯仰力矩气动力合力矩在气流坐标轴系内3.1。2.7pitchingmomentinair一pathaxis从绕y.轴的分童system气流轴俯仰力矩系数M./}合，VZS二{3.1.2.8pitchingmomentcoefficientinalr-C。式中户，v，5的含义同3.1.2.2;。^pathaxissystem为机翼平均气动弦长一{气流轴偏航(方向)力矩气动力合力矩在气流坐标轴系内3.1。2.9yawingmomentinalr一PathaxisN.绕2。轴的分量systern气流轴偏航(方向)力矩系数N·/(专产25“!3.12.10yawingmomentcoefficientinalr-Coa式中P，v，5的含义同3.1.2·2;bpathaxlssystem为机翼展长气流轴滚转力矩气动力合力矩在气流坐标轴系内3.1.2.11rollingmomentinair一pathaxisL。绕x。轴的分量system气流轴滚转力矩系数3.1.2.12rollingmomentcoefficientinair-L·/(告*VZS”{Clapathaxlssystem式中p，v，5，b的含义同3.1.2.10免费标准下载网(www.freebz.net)无需注册即可下载 免费标准下载网(www.freebz.net)GB/T16638.4-1996机体坐标轴系的空气动力、力矩及其系数编号语定义或说明符号R"沿机体坐标轴系竖轴z负方法向力3.1.3.向的分量。机体坐标轴系定义见normalforceGB/T16638.2中2.1.33.1.3.2法向力系数、/(告pws)normalforcecoefficient式中p,V,S的含义同3.1.2.2轴向力R"沿机体坐标轴系纵轴r负方3.1.3.axialforce向的分量3.1.3.轴向力系数，/(合PV"S一axialforcecoefficient式中p,V,S的含义同3.1.2.2横向力R}沿机体坐标轴系横轴Y的分3.1.3.5transverseforce,sideforce量横向力系数3.1.3.transverseforcecoefficient,side:/{合PV,S{CYforcecoefficient式中p,V,S的含义同3.1.2.2俯仰力矩气动力合力矩在机体坐标轴系中绕3.1.3.7pitchingmomentY轴的分量俯仰力矩系数可}合pV2ScqCm3.1.3pitchingmomentcoefficient式中p,V,S,c、的含义同3.1.2.8偏航(方向)力矩气动力合力矩在机体坐标轴系中绕3.1.3.9yawtn只moment二轴的分量偏航(方向)力矩系数动12pV"Sb3.1.3.10yawingmomentcoefficient式中p,V,S,b的含义同3.1.2.10滚转力矩气动力合力矩在机体坐标轴系中绕3.1.3.11rollingmoment二轴的分量滚转力矩系数:/一告pV"Sb3.1.3.12rollingmomentcoefficient式中p,V,S,b的含义同3.1.2.12半机体坐标轴系的空气动力、力矩及其系数标准分享网www.bzfxw.com免费下载免费标准下载网(www.freebz.net)无需注册即可下载 免费标准下载网(www.freebz.net)GB/T16638.4-1996编号术语定义或说明符号R"沿半机体坐标轴系z。轴(即z,半体轴升力轴)负方向的分量。3.1.4.1L.(=L)liftinintermediateaxissystem半机体坐标轴系定义见GB/T16638.2中2.1.5半体轴升力系数3.1.4.2liftcoefficientinintermediateaxisL/I告PwS)C卜式中p,V,S的含义同3.1.2.2system半体轴阻力R"沿半机体坐标轴系z，轴负方3.1.4.3D.draginintermediateaxissystem向的分量半体轴阻力系数3.1.4.4dragcoefficientinintermediate。/(告PV"S)Cnaxissystem式中p,V,S的含义同3.1.2.2半体轴横向力R"沿半机体坐标轴Y方向(即3.1.4..-,transverseforce,sideforceinY(二Y)机体轴系Y方向)的分量intermediateaxissystem半体轴横向力系数transverseforcecoefficient,Y/I告pVS3.1.4.6Cvsideforcecoefficientinintermedi-式中p,V,S的含义同3.1.2.2.ateaxissystem半体轴俯仰力矩气动力合力矩在半机体坐标轴系中3.1.4.7pitchingmomentinintermediateM.二(M)绕Y.轴(即Y轴)的分量axissystem半体轴俯仰力矩系数3.1.4.8pitchingmomentcoefficientin可(合pv"Sc,C。intermediateaxissystem式中p,V,S,c;的含义同3.1.2.8半体轴偏航(方向)力矩气动力合力矩在半机体坐标轴中绕3.1.4.9yawingmomentinintermediateN;(=N.)z.轴(即z。轴)的分量axissystem半体轴偏航(方向)力矩系数3.1.4.10yawingmomentcoefficientinin-N;/(合pV"Sb)Co,(=C..)termediateaxissystem式中p,V,S,b的含义同3.1.2.10免费标准下载网(www.freebz.net)无需注册即可下载 免费标准下载网(www.freebz.net)GB/T16638.4-1996编号术语定义或说明符号半体轴滚转力矩气动力合力矩在半机体坐标轴中绕3.1.4.11rollingmomentinintermediateL二。轴的分量axissystem半体轴滚转力矩系数3.1.4.12rollingmomentcoefficientininter-列2pV}Sb)Cmediate式中p,V,S,b的含义同3.1.2.12axissystem作用在操纵面上的力、力矩及其系数编号术语定义或说明符号作用在飞行器操纵面上的气动力气动铰链力矩3.1.5.1绕其铰链轴的力矩。使操纵面产生Mhaerodynamichingemoment正向偏转的力矩为正气动铰链力矩系数‘/(合pV2SI"3.1.5.2aerodynamichingemomentcoeffi-式中p为自由流密度，V为自由流Chcient速度，S为参考面积，l为参考长度升降舵气动铰链力矩作用在飞行器升降舵上的气动力3.1.5.3aerodynamichingemomentofele-Mhe绕其铰链轴的力矩vator升降舵气动铰链力矩系数3.1.5.4aerodynamichingemomentcoeffi-‘/(告pV"SICh,cientofelevator方向舵气动铰链力矩作用在方向舵舵面上的气动力绕3.1.5.5aerodynamichingemomentofrud-M.其铰链轴的力矩der方向舵气动铰链力矩系数3.1.5.6aerodynamichingemomentcoeffi-‘·/(2pV"SI"C卜rcientofrudder副翼气动铰链力矩作用在飞行器副翼上的气动力绕3.1.5.7aerodynamichingemomentofMh.其铰链轴的力矩aileron标准分享网www.bzfxw.com免费下载免费标准下载网(www.freebz.net)无需注册即可下载 免费标准下载网(www.freebz.net)GB/"r16638.4-1996编号术语定义或说明一}符号{副翼气动力铰链力矩系数}一3.1.5.8aerodynamichingemomentcoeffi-M,./I合PV0S1IC,=cientofaileron3.2空气动力导数3.2.1空气动力静导数编号术语定义或说明符号升力系数对迎角的导数〔升力线斜率)3.2.1.1derivativeofliftcoefficientwith芯I/lC,.orespecttoangleofattack(slopofliftcurve)阻力系数对迎角的导数3.2.1.2derivativeofdragcoefficientwith,)C洲.Cnorespecttoangleofattack法向力系数对迎角的导数3.2.1.3derivativeofnormalforcewithre-X，/;3r〔’、specttoangleofattack轴向力系数对迎角的导数一3.2.1.4derivativeofaxialforcecoefficient斑、,/,)a一withrespecttoangleofattack一一一一一d俯er‘印iv”at矩ive系o数fp对it迎chi角ng的m导o数mentco-一}3.“·‘5{efficientwithrespecttoangleof一一ttackl一I横向力系数对侧滑角的导数3.2.1.6derivativeofsideforcecoefficient}Cr/明CY,withrespecttoangleofsideslip{偏航(方向)力矩系数对侧滑角的导一一数3.2.1.7derivativeofyawingmomentcoef-dC./dPC.dficientwithrespecttoangleofsideslip免费标准下载网(www.freebz.net)无需注册即可下载 免费标准下载网(www.freebz.net)GB/T16638.4-1996编号术语定义或说明符号滚转力矩系数对侧滑角的导数dervativeofrollingmomentcoeffi-3.2.1.8aC,/agC,acientwithrespecttoangleofsideslip升力系数对马赫数的导数3.2.1.9derivativeofliftcoefficientwithac,八7MC-respecttoMachnumber阻力系数对马赫数的导数3.2.1.10derivativeofdragcoefficientwithacn/amCnmrespecttoMachnumber俯仰力矩系数对马赫数的导数derivativeofpitchingmomentco-3.2.1.11a稿八3MC..efficientwithrespecttoMachnumber俯仰力矩系数对升力系数的导数aCm/aG_derivativeofpitchingmomentco,3.2.1.12(当S,二常数)C.1-efficientwithrespecttoliftcoeffi-Se为升降舵偏角cient俯仰静稳定裕量一￡m/刃,_3.2.1.13-Cmc,_pitchingstaticmargin(S.二常数)C。。+(C、/产)式中C，见3.2.2.10,纵向机动性裕量P,=2m/PSc=3.2.1.14longitudinalmaneuvermargin式中阴为飞行器质量，P为自由流密度，S为机翼参考面积,c、为机翼平均气动弦长纵向静稳定导数3.2.1.15longitudinalstaticstabilityderiva-包括有C，，(〕侧刃_tives航向静稳定导数3.2.1.16ac./agC.,yawingstaticstabilityderivative标准分享网www.bzfxw.com免费下载免费标准下载网(www.freebz.net)无需注册即可下载 免费标准下载网(www.freebz.net)GB/T16638.4一1996编号术语定义或说明符号}横向静稳定导数3.2.1。17一，，‘ng一‘一b“‘，yd一‘二芜、/明C、召」;军:)，一，一1·slabl;ltyderlva_3.2.2空气动力动导数编号术语定义或说明符号"l升力系数对无因次迎角变化率的导数肥1/刁‘3.2.2.1derivativeofliftcoefficientwith式中石=(da/d，)(c^/Zv).‘一;为机C恤resPecttothenormalizedrateof翼平均气动弦长.v为自由流速度changeofangleofattack阻力系数对无因次迎角变化率的导一一数刃l)j刁a3。2.2.2derivatlveofdragcoefficientwithC。。式中‘=(da/dt)(c、/ZV)resPecttothenormalizedrateofchangeofangleofattack俯仰力矩系数对无因次迎角变化率的导数derivatlveofpitchingmomentco-汉。/J反3.2.2。3C、efficientwithresPecttothenor-式中云=(da/dt、(。、/Zu)malizedrateofchangeofangleofattack甲~--—l侧力系数对无因次侧滑角变化率的!}导数I「淤飞/刁月{derivatlveofcross一strcamforceco-3.2.2.4(、〔二efflcientwlthresPecttothenor-式中月=(d月/dt)(b/ZV)，b为机n飞allzedrateofchangeofangleof翼展长sldesllp横向力系数对无因次侧滑角变化率!的导数苏丫/刁月3.2.2.5derlvativeofsideforcecoefflcient一。丫公withrespecttothenormallzedrate式中口=(d月/dt)(b/ZV).一ofchangeofangleofsldesllp一}免费标准下载网(www.freebz.net)无需注册即可下载 免费标准下载网(www.freebz.net)GB/T16638.4-1996编号术语定义或说明符号一一偏航(方向)力矩系数对无因次侧滑角变化率的导数derivativeofyawingmomentcoef-aC/dp3.2.2.6C=aficientwithrespecttothenormal-式中9-(d月/dt)(b/2V)izedrateofchangeofangleofsideslip滚转力矩系数对无因次侧滑角变化率的导数derivativeofrollingmomentcoef-刃/0i73.2.2.7Caficientwithrespecttothenormal-式中Q=(d夕/dt)(b/2V)izedrateofchangeofangleofsideslip升力系数对无因次俯仰角速度的导工1/丙数式中q=q(ca/2V),q为俯仰角速3.2.2.8derivativeofliftcoefficientwith度，见GB/T16638.2中2.4.2.3.CU,respecttothenormalizedrateof‘;为机翼平均气动弦长，v为自由pitch流速度阻力系数对无因次俯仰角速度的导数dC/丙3.2.2.9derivativeofdragcoefficientwithCrx,式中q=q(cn/2V)respecttothenormalizedrateofpitch俯仰力矩系数对无因次俯仰角速度的导数,)C耐a73.2.2.10derivativeofpitchingmomentco-CM,一式中q=q(c,,/2V)efficientwithrespecttothenor-}malizedrateofpitch}侧力系数对无因次偏航角速度的导一万数一、/、一一3.2.2.11derivativeoftransverseforcecoef-{式中r=r(bl2V).r为偏航角速Caficientwithrespecttothenormal-izedrateofyaw一度’见GB/T16638.2中2.4.2.4}横向力系数对无因次偏航角速度的{导数刃Yl厉3.2.2.12derivativeofsideforcecoefficientCY,式中r=r(b/2V)withrespecttothenormalizedrateofyaw标准分享网www.bzfxw.com免费下载免费标准下载网(www.freebz.net)无需注册即可下载 免费标准下载网(www.freebz.net)GB/T16638.4-1996编号术语定义或说明符号滚转力矩系数对无因次偏航角速度的导数劣Ja3.2.2.13derivativeofrollingmomentcoef-C式中r=r(b/2V)ficientwithrespecttothenormal-izedrateofyaw偏航(方向)力矩系数对无因次偏航角速度的导数aCo/ar3.2.2.14derivativeofyawingmomentcoef-C=.式中r=r(b/2V)ficientwithrespecttothenormal-izedrateofyaw侧力系数对无因次滚转角速度的导dCc/币数式中p=p(02V),p为滚转角速3.2.2.15derivativeofcross-streamforceco-Cc,度，见GB/T16638.2中2.4.2.2,befficientwithrespecttothenor-为机翼展长，V为自由流速度malizedrateofroll横向力系数对无因次滚转角速度的导数acY/ap3.2.2.16derivativeofsideforcecoefficientCYp式中p=p(02V)withrespecttothenormalizedrateofroll滚转力矩系数对无因次滚转角速度的导数aC/ap3.2.2.17derivativeofrollingmomentcoef-CP式中p=p(02V)ficientwithrespecttothenormal-}一，zedrateofroll偏航(方向)力矩系数对无因次滚转角速度的导数aC./ap3.2.2.18derivativeofyawingmomentcoef-Cp式中p=p(02V)ficientwithrespecttothenormal-izedrateofroll俯仰阻尼导数即俯仰力矩系数对无因次俯仰角3.2.2.19Cm,pitchingdampingderivatives速度的导数滚转阻尼导数即滚转力矩系数对无因次滚转角3.2.2.20C,prollingdampingderivatives速度的导数偏航阻尼导数即偏航(方向)力矩系数对无因次3.2.2.21C=yawingdampingderivatives偏航角速度的导数免费标准下载网(www.freebz.net)无需注册即可下载 免费标准下载网(www.freebz.net)GB/T16638.4-1996编号语定义或说明符号CC必俯仰力矩系数对无因次迎角变化n率的导数洗流时差动导数-，滚转力矩系数对无因次侧滑角变‘3.2.2.22timedelydynamicderivativeswash化率的导数偏航(方向)力矩系数对无因次侧C=.a滑角变化率的导数滚转力矩系数对无因次偏航角速C交又动导数度的导数3.2.2.23crossdynamicderivatives偏航(方向)力矩系数对无因次滚〔’。p转角速度的导数3.2.3空气动力操纵导数}编号术语定义或说明符号一升力系数对升降舵偏角的导数工1/d6derivativeofliftcoefficientwith3.2.3.1式中81为升降舵偏角，见CLa}respecttothedeflectionofeleva-GB/T16638.2中2.5.1tor俯仰力矩系数对升降舵(平尾)偏角的导数dom/泌3.2.3.2derivativeofpitchingmornentco-(一，e<(C.").efficientwithrespecttothedeflec-{即升降舵(平尾躁纵效率(d7./dip)tionofelevator(horizontaltail){{一升力系数又，无因次升降舵偏转角速一、/。、{!度的导数一_3.2.3.3derivativeofliftcoefficientwith式中a=一(dr5,/dt)(cn/2V),S,为Csrespecttothenormalizedrateof}升降舵偏角，CA为机翼平均气动deflectionofelevator」弦，V为自由流速度阻力系数对无因次升降舵偏转角速一度的导数一、/刁、一3.2.3.4derivativesofdragcoefficientwithrespecttonormalizedrateofde-一式中S一dc)‘二/2V)Electionofelevator}}l标准分享网www.bzfxw.com免费下载免费标准下载网(www.freebz.net)无需注册即可下载 免费标准下载网(www.freebz.net)GB/T16638.4-1996编号术语定义或说明符号俯仰力矩系数对无因次升降舵偏转角速度的导数derivativeofpitchingmomentco-3Cm/aSr3.2.3.5Cma.efficientwithrespecttothenor-式中.a,=(daddt)(cn/2V)malizedrateofdeflectionofeleva-tor侧力系数对方向舵偏角的导数dCc/dBrderivativeofcross-streamforceco-3.2.3.6式中Sr为方向舵偏角，见Ccarefficientwithrespecttothedeflec-GB/T16638.2中2.5.3tionofrudder滚转力矩系数对方向舵偏角的导数derivativeofrollingmomentcoef-3.2.3.7ac,lasrCIL,ficientwithrespecttothedeflec-tionofrudder偏航(方向)力矩系数对方向舵偏角的导数即方向舵操纵效率亡}ar3.2.3.8derivativeofyawingmomentcoef-r./韶rficientwithrespecttothedeflec-tionofrudder侧力系数对无因次方向舵偏转角速度的导数ac,/刁S.3.2.3.9derivativeofcross-streamforceco-Ccsr式中S,=(dSr/dt)(b/2V),b为机efficientwithrespecttothenor-翼展长，V为自由流速度malizedrateofdeflectionofrudder滚转力矩系数对无因次方向舵偏转角速度的导数aG/aSr3.2.3.10derivativeofrollingmomentcoef-Cibrficientwithrespecttothenormal-式中Sr=(d8r/dt)(b/2V)izedrateofdeflectionofrudder偏航(方向)力矩系数对无因次方向舵偏转角速度的导数,r}/as,3.2.3.11derivativeofyawingmomentcoef-认;ficientwithrespecttothenormal-式中a,=(d8,/dt)(b/2V)izedrateofdeflectionofrudder免费标准下载网(www.freebz.net)无需注册即可下载 免费标准下载网(www.freebz.net)GB/T16638.4-1996编号术语定义或说明符号侧力系数对副翼偏角的导数acc/武derivativeofcross-streamforceco-3.2.3.12式中S.为副翼偏角，见Cca.efficientwithrespecttothedeflec-GB/T16638.2中2.5.6tionofaileron滚转力矩系数对副翼偏角的导数derivativeofrollingmomentcoef-即副翼操纵效率3.2.3.13C】‘ficientwithrespecttothedeflec-刃/as.tionofaileron偏航(方向)力矩系数对副界偏角的导数3.2.3.14derivativeofyawingmomentcoef-acdaa.C.=ficientwithrespecttothedeflec-tionofaileron侧力系数对无因次副典偏转角速度的导数X",/aS.3.2.3.15derivativeofcross-streamforceco-Cc;.efficientwithrespecttothenor-式中S。二(dS./dt)(b/2V)malizedrateofdeflectionofaileron滚转力矩系数对无因次副翼偏转角速度的导数ac/aS.3.2.3.16derivativeofrollingmomentcoef-Cie.ficientwithrespecttothenormal-式中S.=(d8./dt)(b/2V)izedrateofdeflectionofaileron偏航(方向)力矩系数对无因次副翼偏转角速度的导数aC./aS.3.2.3.17derivativeofyawingmomentcoef-C.-ficientwithrespecttothenormal-式中S。二(d6,/dt)(b/2V)izedrateofdeflectionofaileron13标准分享网www.bzfxw.com免费下载免费标准下载网(www.freebz.net)无需注册即可下载 免费标准下载网(www.freebz.net)GB/T16638.4-1996汉语索引(按汉语拼音顺序编排)方向舵气动铰链力矩3.1.5.5俯仰静稳定裕量3.2.1.13半体轴俯仰力矩3.1.4.7俯仰力矩系数3.1.3.8半体轴滚转力矩3.1.4.11俯仰力矩系数对升降舵偏角的导数3.2.3.2半体轴横向力3.1.4.5俯仰力矩系数对无因次俯仰角速度的半体轴偏航(方向)力矩3.1.4.9导数3.2.2.10半体轴升力3.1.4.1俯仰力矩系数对无因次迎角变化率的半体轴阻力3.1.4.3导数3.2.2.3半体轴俯仰力矩系数3.1.4.8俯仰阻尼导数3.2.2.19半体轴滚转力矩系数3.1.4.12副翼气动铰链力矩系数3.1.5.8半体轴横向力系数3.1.4.6半体轴偏航(方向)力矩系数3.1.4.10半体轴升力系数3.1.4.2滚转力矩3.1.3.11半体轴阻力系数3.1.4.4滚转力矩系数对侧滑角的导数3.2.1.8滚转力矩系数对副翼偏角的导数3.2.3.13滚转力矩系数对无因次方向舵偏转角速度的导数3.2.3.10侧力3.1.2.5侧力系数对方向舵偏角的导数3.2.3.6滚转力矩系数对无因次滚转角速度的侧力系数对无因次侧滑角变化率的导数3.2.2.4导数3.2.2.17侧力系数对无因次副翼偏转角速度的导数滚转阻尼导数3.2.2.203.2.3.15滚转力矩系数3.1.3.12侧力系数3.1.2.6滚转力矩系数对方向舵偏角的导数3.2.3.7侧力系数对副翼偏角的导数3.2.3.12滚转力矩系数对无因次侧滑角变化率侧力系数对Ii,ftl次方向舵偏转角速度的导数3.2.2.7的导数3.2.3.9滚转力矩系数对无因次副翼偏转角速侧力系数对尤因次i转角速度的导数3.2.2.15度的导数3.2.3.16滚转力矩系数对无因次偏航角速度的导数3.2.2.13法向力3.1.3.1法向力系数刊迎角的导数3.2.1.3方向呢气动铰链力矩系数3.1.5.6航向静稳定导数3.2.1.16{府{印力}_3.1.3.7横向力3.1.3.5俯仰力矩系t林寸马赫数的导数3.2.1.11横向力系数对侧滑角的导数3.2.1.6俯仰力矩系数时什力系数的导数3.2.1.12横向力系数对无因次滚转角速度的导数3.2.2.16俯仰力矩系数对无因次升降舵偏转角横向静稳定导数3.2.1.17速度的导数3.2.3.5横向力系数3.1.3.6俯仰力矩系数对迎角的导数3.2.1.5横向力系数对无因次侧滑角变化率的副翼气动铰链力矩3.1.5.7导数3.2.2.5法向力系数3l.3.2横向力系数对无因次偏航角速度的导数3.2.2.12免费标准下载网(www.freebz.net)无需注册即可下载 免费标准下载网(www.freebz.net)GB/T16638.4-1996气动轴滚转力矩系数3.1.2.12气动轴偏航(方向)力矩系数3.1.2.10交叉动导数3.2.2.23升降舵气动铰链力矩3.1.5.3空气动力合力3.1.1升力3.1.2.1空气动力合力矩升力系数对马赫数的导数3.2.1.9升力系数对无因次俯仰角速度的导数3.2.2.8升力系数对无因次迎角变化率的导数3.2.2.1偏航(方向)力矩3.1.3.9时差动导数3.2.2.22偏航(方向)力矩系数对侧滑角的导数3.2.1.7升降舵气动铰链力矩系数3.1.5.4偏航(方向)力矩系数对副翼偏角的导数3.2.3.14升力系数3.1.2.2偏航(方向)力矩系数对无因次副翼偏升力系数对升降舵偏角的导数3.2.3.1转角速度的导数3.2.3.17升力系数对无因次升降舵偏转角速度偏航(方向)力矩系数对无因次偏航角的导数3.2.3.3速度的导数3.2.2.14升力系数对迎角的导数(升力线斜率)3.2.1.1偏航(方向)力矩系数3.1.3.10偏航(方向)力矩系数对方向舵偏角的导数3.2.3.8轴向力3.1.3.3偏航(方向)力矩系数对无因次侧滑角变轴向力系数对迎角的导数3.2.1.4化率的导数3.2.3.11阻力系数3.1.2.4偏航(方向)力矩系数对无因次滚转角速阻力系数对无因次俯仰角速度的导数3.2.2.9度的导数3.2.2.18阻力系数对无因次迎角变化率的导数3.2.2.2偏航(方向)阻尼导数3.2.2.21纵向机动性裕量3.2.1.14轴向力系数3.1.3.4阻力3.1.2.3气动铰链力矩，3.1.5.1阻力系数对马赫数的导数3.2.1.10气动轴俯仰力矩3.1.2.7阻力系数对无因次升降舵偏转角速度气动轴滚转力矩3.1.2.11的导数3.2.3.4气动轴偏航(方向)力矩3.1.2.9阻力系数对迎角的导数3.2.1.2气动铰链力矩系数3.1.5.2纵向静稳定导数3.2.1.15气动轴俯仰力矩系数3.1.2.8标准分享网www.bzfxw.com免费下载免费标准下载网(www.freebz.net)无需注册即可下载 免费标准下载网(www.freebz.net)Gs/T16638.4-1996英文索引(按英文字母顺序编排)Aaerodynamichingemoment3.1.5.1aerodynamichingemomentcoefficient3.1.5.2aerodynamichingemomentcoefficientofaileron3.1.5.8aerodynamichingemomentcoefficientofelevator3.1.5.4aerodynamichingemomentcoefficientofrudder3.1.5.6aerodynamichingemomentofaileron3.1.5.7aerodynamichingemomentofelevator3.1..5.3aerodynamichingemomentofrudder3.1.5.5aerodynamicresultantforce3.1.1.1aerodynamicresultantmoment3.1.1.2axialforce3.1.3.3axialforcecoefficient3.1.3.4Ccrossdynamicderivatives3.2.2.23cross-streamforce3.1.2.5cross-streamforcecoefficient3.1.2.6Dderivativeofaxialforcecoefficienttwithrespecttoangleofattack3.2.1.4derivativeofcross-streamforcecoefficientwithrespecttothedeflectionofaileron3.2.3.12derivativeofcross-streamforcecoefficientwithrespecttothedeflectionofrudder3.2.3.6derivativeofcross-streamforcecoefficientwithrespecttothenormalizedrateofchangeofangleofsideslip3.2.2月derivativeofcross-streamforcecoefficientwithrespecttothenormalizedrateofdeflectionofaileron3.2.3.15derivativeofcrossstreamforcecoefficientwithrespecttothenormalizedrateofdeflectionofrudder3.2.3.9derivativeofcross-streamforcecoefficientwithrespecttothenormalizedrateofroll3.2.2.15derivative(fdragcoefficientwithrespecttoangleofattack3.2.1.2derivativeofdragcoefficientwithrespecttoMuchnumber3.2.1.10derivativeofdragcoefficientwithrespecttothenormalizedrateofchangeofangleofattack3.2.2.2derivativeofdragcoefficientwithrespecttothenormalizedrateofdeflectionofelevator3.2.3.4derivativeofdragcoefficientwithrespecttothenormalizedrateofpitch3.2.2.9derivativeofliftcoefficientwithrespecttoangleofattack(slopofliftcurve)3.2.1.1derivativeofliftcoefficientwithrespecttoMuchnumber3.2.1.9derivativeofliftcoefficientwithrespecttothedeflectionofelevator3.2.3.116免费标准下载网(www.freebz.net)无需注册即可下载 免费标准下载网(www.freebz.net)cs/T16638.4-1996derivativeofliftcoefficientwithrespecttothenormalizedrateofchangeofangleofattack3.2.2.1derivativeofliftcoefficientwithrespecttothenormalizedrateofdeflectionofelevator3.2.3.3derivativeofliftcoefficientwithrespecttothenormalizedrateofpitch3.2.2.8derivativeofnormalforcewithrespecttoangleofattack3.2.1.3derivativeofpitchingmomentcoefficientwithrespecttoangleofattack32.1.5derivativeofpitchingmomentcoefficientwithrespecttoliftcoefficient3.2.1.12derivativeofpitchingmomentcoefficientwithrespecttoMuchnumber3.2.1.11derivativeofpitchingmomentcoefficientwithrespecttothedeflectionofelevator3.2.3.2derivativeofpitchingmomentcoefficientwithrespecttothenormalizedrateofchangeofangleofattack3.2.2.3derivativeofpitchingmomentcoefficientwithrespecttothenormalizedrateofdeflectionofelevator3.2.3.5derivativeofpitchingmomentcoefficientwithrespecttothenormalizedrateofpitch3.2.2.10derivativeofrollingmomentcoefficientwithrespecttoangleofsideslip3.2.1.8derivativeofrollingmomentcoefficientwithrespecttothedeflectionofaileron3.2.2.13derivativeofrollingmomentcoefficientwithrespecttothedeflectionofrudder3.2.3.7derivativeofrollingmomentcoefficientwithrespecttothenormalizedrateofchangeofangleofsideslip3.2.2-7derivativeofrollingmomentcoefficientwithrespecttothenormalizedrateofdeflectionofaileron3.2.3.16derivativeofrollingmomentcoefficientwithrespecttothenormalizedrateofdeflectionofrudder3.2.3.10derivativeofrollingmomentcoefficientwithrespecttothenormalizedrateofroll3.2.2.17derivativeofrollingmomentcoefficientwithrespecttothenormalizedrateofyaw3.2.2.13derivativeofsideforcecoefficientwithrespecttoangleofsideslip3.2.1.6derivativeofsideforcecoefficientwithrespecttothenormalizedrateofchangeofangleofsideslip3.2.2。5derivativeofsideforcecoefficientwithrespecttothenormalizedrateofroll3.2.2.16derivativeofsideforcecoefficientwithrespecttothenormalizedrateofyaw3.2.2.12derivativeoftransverseforcecoefficientwithrespecttothenormalizedrateofyaw3.2.2.11derivativeofyawingmomentcoefficientwithrespecttoangleofsideslip3.2.1.7derivativeofyawingmomentcoefficientwithrespecttothedeflectionofaileron3.2.3.14derivativeofyawingmomentcoefficientwithrespecttothedeflectionofrudder3.2.3.8derivativeofyawingmomentcoefficientwithrespecttothenormalizedrateofchangeofangleofsideslip3.2.2.6derivativeofyawingmomentcoefficientwithrespecttothenormalizedrateofdeflectionofaileron3.2.3.17derivativeofyawingmomentcoefficientwithrespecttothenormalizedrateofdeflectionofrudder3.2.3.11derivativeofyawingmomentcoefficientwithrespecttothenormalizedrateofroll3.2.2.18derivativeofyawingmomentcoefficientwithrespecttothenormalizedrateofyaw3.2.2.14drag3.1.2.3dragcoefficient3.1.2.417标准分享网www.bzfxw.com免费下载免费标准下载网(www.freebz.net)无需注册即可下载 免费标准下载网(www.freebz.net)ca/T16638.4-1996dragcoefficientinintermediateaxissystem3.1.4.4draginintermediateaxissystem3.1.4.31Jlift3.1.2.1liftcoefficient3.1.2.2liftcoefficientinintermediateaxissystem3.1.4.2liftinintermediateaxissystem3.1.4.1longitudinalmaneuvermargin3.2.1.14longitudinalstaticstabilityderivatives3.2.1.15Nnormalforce3.1.3.1normalforcecoefficient3.1.3.2Ppitchingdampingderivatives3.2.2.19pitchingmoment3.1.3.7pitchingmomentcoefficient3.1.3.8pitchingmomentcoefficientinair-pathakissystem3.1.2.8pitchingmomentcoefficientinintermediateaxissystem.3.1.4.8pitchingmomentinair-pathaxissystem3.1.2.7pitchingmomentinintermediateaxissystem3.1.4.7pitchingstaticmargin3.2.1.13Rrollingdampingderivatives3.2.2.20rollingmoment3.1.3.11rollingmomentcoefficient3.1.3.12rollingmomentcoefficientinair-pathaxissystem3.1.2.12rollingmomentcoefficientinintermediateaxissystem3.1.4.121lrollingmomentinair-pathaxissystem3.1.2.1lrollingmomentinintermediateaxissystem3。1.4.rollingstaticstabilityderivative(lateralstaticstabilityderivative)3.2.1.17Tortransverseforcesideforce3.1.3.5ortransverseforcesideforceinintermediateaxissystem3.1.4.5transverseforcecoefficientorsideforcecoefficient3.1.3.6transverseforcecoefficientinintermediateaxissystem3.1.4.6Yyawingdampingderivatives3.2.2.2118免费标准下载网(www.freebz.net)无需注册即可下载 免费标准下载网(www.freebz.net)cs/T16638.4-19963.1.3.9yawingmomentyawingmomentcoefficient3.1.3.10yawingmomentcoefficientinair-pathaxissystem3.1.2.10yawingmomentcoefficientinintermediateaxissystem3.1.4.10yawingmomentinair-pathaxissystem3.1.2.9yawingmomentinintermediateaxissystem3.1.4.9yawingstaticstabilityderivative3.2.1.16标准分享网www.bzfxw.com免费下载免费标准下载网(www.freebz.net)无需注册即可下载'