CN102661729B - Method for confirming sectional dimension of I-shaped hollow beam of high-speed fluttering model of airplane - Google Patents

Method for confirming sectional dimension of I-shaped hollow beam of high-speed fluttering model of airplane Download PDF

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CN102661729B
CN102661729B CN201210146167.XA CN201210146167A CN102661729B CN 102661729 B CN102661729 B CN 102661729B CN 201210146167 A CN201210146167 A CN 201210146167A CN 102661729 B CN102661729 B CN 102661729B
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罗务揆
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Abstract

本发明属于结构力学领域,涉及一种飞机高速颤振模型工字形空心梁截面尺寸的确定方法。其特征在于,确定带四个耳片薄壁矩形空心梁截面尺寸的步骤如下:计算薄壁矩形空心梁在具有预定数值的垂直向惯性矩Ix和极惯性矩J以及壁厚为t的矩形等效宽度a1和等效高度b1;对预定的极惯性矩J进行调整;计算等效宽度a2和等效高度b2;以b2为b3的最大值范围,迭代得到符合截面特性控制方程的截面尺寸a3,b3和L3。本发明提高了模型截面设计的精度,减少了模型设计的不确定性,缩短了确定截面尺寸的时间,提高了颤振模型的设计效率,并且由于耳片处于矩形的四个角点,降低了截面的总高度,在一定程度上满足了尺寸限制要求。

The invention belongs to the field of structural mechanics and relates to a method for determining the section size of an I-shaped hollow beam of an aircraft high-speed flutter model. It is characterized in that, the step of determining the section size of the thin-walled rectangular hollow beam with four lugs is as follows: calculate the vertical moment of inertia Ix and the polar moment of inertia J of the thin-walled rectangular hollow beam with a predetermined value and the rectangular wall thickness t Equivalent width a 1 and equivalent height b 1 ; adjust the predetermined polar moment of inertia J; calculate equivalent width a 2 and equivalent height b 2 ; take b 2 as the maximum range of b 3 , iteratively obtain the cross section The characteristic governing equations are the section dimensions a 3 , b 3 and L 3 . The invention improves the accuracy of model section design, reduces the uncertainty of model design, shortens the time for determining the section size, improves the design efficiency of the flutter model, and reduces the The overall height of the section satisfies the size restriction to a certain extent.

Description

一种飞机高速颤振模型工字形空心梁截面尺寸的确定方法A Method for Determining the Section Dimensions of I-shaped Hollow Beams of Aircraft High-speed Flutter Model

技术领域technical field

本发明属于结构力学领域,涉及一种飞机高速颤振模型工字形空心梁截面尺寸的确定方法。The invention belongs to the field of structural mechanics and relates to a method for determining the section size of an I-shaped hollow beam of an aircraft high-speed flutter model.

背景技术Background technique

高速颤振模型可以用来获取飞机及其部件的跨声速颤振特性,而高速颤振模型通常需要很小的梁架质量来提供很大的翼面刚度,而为了可以满足三向刚度的设计要求,带耳片的矩形薄壁空心梁截面是一个理想的设计形式。The high-speed flutter model can be used to obtain the transonic flutter characteristics of the aircraft and its components, and the high-speed flutter model usually requires a small beam mass to provide a large airfoil stiffness, and in order to meet the three-dimensional stiffness design Rectangular thin-walled hollow beam section with lugs is an ideal design form.

以前通常需要通过试凑的方法获取满足要求的截面尺寸。试凑的方法有如下缺点:第一、调整截面尺寸数据需要设计人员的经验,凭经验给出的尺寸数据往往误差很大,甚至会出现很难调整出满足设计要求的尺寸的情况,影响模型截面刚度的精度,增加了模型设计的不确定性;第二、通过试凑法要确定截面尺寸,需要进行多轮次的人工调整和判断,时间长,效率低,严重影响模型设计周期。In the past, it was usually necessary to obtain the required section size by trial and error. The trial and error method has the following disadvantages: First, the adjustment of the section size data requires the experience of the designer, and the size data given by experience often has a large error, and it may even be difficult to adjust the size that meets the design requirements, which affects the model. The accuracy of the section stiffness increases the uncertainty of the model design; second, to determine the section size through the trial and error method, multiple rounds of manual adjustment and judgment are required, which takes a long time and low efficiency, seriously affecting the model design cycle.

参见中国专利《带耳片薄壁矩形空心梁截面尺寸的确定方法》(申请号201110232656.2),在保证带耳片矩形薄壁空心梁具有预定数值的垂直向惯性矩Ix、侧向惯性矩Iy和极惯性矩J以及壁厚和耳片厚度均为t的情况下,可直接确定其矩形的等效宽度a、等效高度b和空心梁截面总宽L,这种方法不需要试凑,而且精度和效率都很高。但这种方法对应的截面的特点是耳片位于截面的中性面上,这种截面有可能会因为等效高度b值过大而带来模型设计及加工上的麻烦。Refer to the Chinese patent "Method for Determining Sectional Dimensions of Thin-walled Rectangular Hollow Beams with Ears" (Application No. 201110232656.2), in order to ensure that the rectangular thin-walled hollow beams with ears have predetermined values of vertical moment of inertia I x and lateral moment of inertia I When y , polar moment of inertia J, and wall thickness and lug thickness are both t, the equivalent width a, equivalent height b, and total width L of the hollow beam section can be directly determined. This method does not require trial and error , with high accuracy and efficiency. However, the characteristic of the section corresponding to this method is that the lugs are located on the neutral plane of the section. This kind of section may cause troubles in model design and processing because the equivalent height b value is too large.

发明内容Contents of the invention

本发明的目的是:提出一种飞机高速颤振模型工字形空心梁截面尺寸的确定方法,以提高模型截面刚度的精度,减少模型设计的不确定性,缩短确定截面尺寸的时间,提高颤振模型的设计效率,并且本发明提出的带四个耳片的薄壁矩形空心梁的耳片位于矩形的四个角点,在相同截面特性目标值的条件下,有效地降低了截面的总高度。The purpose of the present invention is: to propose a method for determining the section size of an I-shaped hollow beam of an aircraft high-speed flutter model, to improve the accuracy of the model section stiffness, reduce the uncertainty of model design, shorten the time for determining the section size, and improve flutter The design efficiency of the model, and the lugs of the thin-walled rectangular hollow beam with four lugs proposed by the present invention are located at the four corners of the rectangle, and under the condition of the same section characteristic target value, the total height of the section is effectively reduced .

本发明的技术解决方案是:飞机高速颤振模型工字形空心梁截面尺寸的确定方法,在保证飞机高速颤振模型工字形空心梁具有预定数值的垂直向惯性矩Ix、侧向惯性矩Iy和极惯性矩J以及矩形薄壁空心梁壁厚为t以及耳片厚度为tr的情况下,确定其矩形的等效宽度a3、等效高度b3和空心梁截面总宽L3。这里规定所有的长度单位为mm。其特征在于,确定飞机高速颤振模型工字形空心梁截面尺寸的步骤如下:The technical solution of the present invention is: the method for determining the cross-sectional size of the I-shaped hollow beam of the high-speed flutter model of the aircraft, after ensuring that the I-shaped hollow beam of the high-speed flutter model of the aircraft has the vertical moment of inertia I x and the lateral moment of inertia I y and the polar moment of inertia J, and when the wall thickness of the rectangular thin-walled hollow beam is t and the thickness of the lug is t r , determine its rectangular equivalent width a 3 , equivalent height b 3 and the total width L 3 of the hollow beam section. All the length units are stipulated here as mm. It is characterized in that the steps of determining the section size of the I-shaped hollow beam of the aircraft high-speed flutter model are as follows:

1、令tr=nrt;1. Let t r =n r t;

2、计算薄壁矩形空心梁在具有预定数值的垂直向惯性矩Ix和极惯性矩J以及矩形薄壁空心梁壁厚为t1以及耳片厚度为tr时的矩形等效宽度a1和等效高度b12. Calculate the rectangular equivalent width a 1 and etc. of the thin-walled rectangular hollow beam when the vertical moment of inertia I x and the polar moment of inertia J of the rectangular thin-walled hollow beam have a predetermined value, and the wall thickness of the rectangular thin-walled hollow beam is t 1 and the thickness of the lug is t r Effective height b 1 :

2.1、根据下式计算第一中间变量p和第二中间变量q:2.1. Calculate the first intermediate variable p and the second intermediate variable q according to the following formula:

pp == 33 tt (( 44 II xx ++ JJ )) qq == 99 II xx tt 22 (( 44 II xx -- JJ )) .. .. .. [[ 11 ]]

2.2、根据下式计算第三中间变量s:2.2. Calculate the third intermediate variable s according to the following formula:

sthe s == 11 22 (( pp -- pp 22 -- 44 qq )) .. .. .. [[ 22 ]]

2.3、计算等效宽度a1和等效高度b12.3. Calculate equivalent width a 1 and equivalent height b 1 :

aa 11 == 22 II xx sthe s 22 tt 33 -- sthe s 33 33 bb 11 == sthe s 33 .. .. .. [[ 33 ]]

3、对预定的极惯性矩J进行调整:根据下式计算出极惯性矩J调整后的值J13. Adjust the predetermined polar moment of inertia J: Calculate the adjusted value J 1 of the polar moment of inertia J according to the following formula:

J1=J[1-tr/(2b1)]……………………………[4]J 1 =J[1-t r /(2b 1 )]………………………[4]

4、计算等效宽度a2和等效高度b2:将公式[1]中的J换成J1,然后按照步骤2所述的方法计算出等效宽度a2和等效高度b24. Calculate the equivalent width a 2 and equivalent height b 2 : replace J in the formula [1] with J 1 , and then calculate the equivalent width a 2 and equivalent height b 2 according to the method described in step 2;

5、迭代计算截面特性控制方程并得到截面尺寸:5. Iteratively calculate the governing equation of the section properties and obtain the section size:

5.1、令b3k=b2-0.1k,变量k=1,2,3,…,int(10b2),其中int()为取整函数;5.1. Let b 3k =b 2 -0.1k, variable k=1,2,3,...,int(10b 2 ), where int() is a rounding function;

5.2、根据b3k计算a3k5.2. Calculate a 3k according to b 3k :

aa 33 kk == JJ 11 // (( 44 tt )) bb 33 kk 22 (( 11 ++ 11 ++ 22 bb 33 kk 33 JJ 11 (( 44 tt )) )) .. .. .. [[ 55 ]]

5.3、根据a3k和b3k计算L3k5.3. Calculate L 3k according to a 3k and b 3k :

LL 33 kk == (( aa 33 kk ++ tt )) ++ 66 II xx // tt -- (( aa 33 kk ++ tt )) (( 33 bb 33 kk 22 ++ tt 22 )) -- (( bb 33 kk -- tt )) 33 nno rr [[ 33 (( bb 33 kk ++ tt -- tt rr )) 22 ++ tt rr 22 ]] .. .. .. [[ 66 ]]

5.4、根据a3k,b3k和L3k计算fk5.4. Calculate f k according to a 3k , b 3k and L 3k :

Figure GDA0000465527970000026
Figure GDA0000465527970000026

5.5、根据fk计算errk5.5. Calculate err k according to f k :

errerr kk == || ff kk -- 66 II ythe y // tt || 66 II ythe y // tt ×× 100100 %% .. .. .. [[ 88 ]]

5.6、获取截面尺寸:5.6. Obtain the section size:

找出误差值errk最小情况对应的a3k和b3k计算L3k,即为最终截面尺寸a3和b3计算L3Find a 3k and b 3k corresponding to the minimum error value err k and calculate L 3k , that is, calculate L 3 for the final cross-sectional dimensions a 3 and b 3 .

本发明的优点是:提高了模型截面刚度的精度,减少了模型设计的不确定性,缩短了确定截面尺寸的时间,提高了颤振模型的设计效率。本发明的一个实施例与目前的试凑方法相比,本发明确定截面尺寸的时间仅为10分钟,而试凑方法需要25小时,本发明的用时仅为试凑方法的一百五十分之一。同时,降低了截面总高度,满足了尺寸约束,给模型设计加工带来了便利。The invention has the advantages of improving the accuracy of the section stiffness of the model, reducing the uncertainty of model design, shortening the time for determining the size of the section, and improving the design efficiency of the flutter model. Compared with the current trial and error method, the present invention only takes 10 minutes to determine the section size, while the trial and error method needs 25 hours, and the time spent by the present invention is only 150 minutes of the trial and error method. one. At the same time, the overall height of the section is reduced to meet the size constraints, which brings convenience to model design and processing.

附图说明Description of drawings

图1是不带耳片的薄壁矩形空心梁的横剖面示意图。图中a1是本发明步骤1所计算的矩形的等效宽度,a1=矩形的外缘宽度-薄壁厚度t。b1是本发明步骤1所计算的矩形的等效高度,b1=矩形的外缘高度-薄壁厚度t。图1中的二维坐标系的原点0为矩形的中心,x轴平行于矩形的宽度方向,正方向朝右,y轴的正方向朝上。Figure 1 is a schematic cross-sectional view of a thin-walled rectangular hollow beam without lugs. In the figure, a 1 is the equivalent width of the rectangle calculated in Step 1 of the present invention, and a 1 = the width of the outer edge of the rectangle-thin-wall thickness t. b 1 is the equivalent height of the rectangle calculated in step 1 of the present invention, b 1 = height of the outer edge of the rectangle - thickness t of the thin wall. The origin 0 of the two-dimensional coordinate system in Figure 1 is the center of the rectangle, the x-axis is parallel to the width direction of the rectangle, the positive direction is to the right, and the positive direction of the y-axis is upward.

图2是飞机高速颤振模型工字形空心梁的横剖面示意图。图2中的二维坐标系与图1相同。Fig. 2 is a cross-sectional schematic diagram of an I-shaped hollow beam of an aircraft high-speed flutter model. The two-dimensional coordinate system in Fig. 2 is the same as that in Fig. 1 .

具体实施方式Detailed ways

下面对本发明做进一步详细说明。参见图1、2,飞机高速颤振模型工字形空心梁截面尺寸的确定方法,在保证飞机高速颤振模型工字形空心梁截面具有预定数值的垂直向惯性矩Ix、侧向惯性矩Iy和极惯性矩J以及矩形薄壁空心梁壁厚为t以及耳片厚度为tr的情况下,确定其矩形的等效宽度a3、等效高度b3和空心梁截面总宽L3。这里规定所有的长度单位为mm。其特征在于,确定飞机高速颤振模型工字形空心梁截面尺寸的步骤如下:The present invention will be described in further detail below. Referring to Figures 1 and 2, the determination method of the section size of the I-shaped hollow beam of the aircraft high-speed flutter model is to ensure that the section of the I-shaped hollow beam of the aircraft high-speed flutter model has a predetermined value of vertical moment of inertia I x and lateral moment of inertia I y And the polar moment of inertia J, the wall thickness of the rectangular thin-walled hollow beam is t, and the thickness of the lug is t r , determine its rectangular equivalent width a 3 , equivalent height b 3 and the total width L 3 of the hollow beam section. All lengths are specified here in mm. It is characterized in that the steps of determining the section size of the I-shaped hollow beam of the aircraft high-speed flutter model are as follows:

1、令tr=nrt;1. Let t r =n r t;

2、计算薄壁矩形空心梁在具有预定数值的垂直向惯性矩Ix和极惯性矩J以及矩形薄壁空心梁壁厚为t1以及耳片厚度为tr时的矩形等效宽度a1和等效高度b12. Calculate the rectangular equivalent width a 1 and etc. of the thin-walled rectangular hollow beam when the vertical moment of inertia I x and the polar moment of inertia J of the rectangular thin-walled hollow beam have a predetermined value, and the wall thickness of the rectangular thin-walled hollow beam is t 1 and the thickness of the lug is t r Effective height b 1 :

2.1、根据下式计算第一中间变量p和第二中间变量q:2.1. Calculate the first intermediate variable p and the second intermediate variable q according to the following formula:

pp == 33 tt (( 44 II xx ++ JJ )) qq == 99 II xx tt 22 (( 44 II xx -- JJ )) .. .. .. [[ 11 ]]

2.2、根据下式计算第三中间变量s:2.2. Calculate the third intermediate variable s according to the following formula:

sthe s == 11 22 (( pp -- pp 22 -- 44 qq )) .. .. .. [[ 22 ]]

2.3、计算等效宽度a1和等效高度b12.3. Calculate equivalent width a 1 and equivalent height b 1 :

aa 11 == 22 II xx sthe s 22 tt 33 -- sthe s 33 33 bb 11 == sthe s 33 .. .. .. [[ 33 ]]

3、对预定的极惯性矩J进行调整:根据下式计算出极惯性矩J调整后的值J13. Adjust the predetermined polar moment of inertia J: Calculate the adjusted value J 1 of the polar moment of inertia J according to the following formula:

J1=J[1-tr/(2b1)]……………………………[4]J 1 =J[1-t r /(2b 1 )]………………………[4]

4、计算等效宽度a2和等效高度b2:将公式[1]中的J换成J1,然后按照步骤2所述的方法计算出等效宽度a2和等效高度b24. Calculate the equivalent width a 2 and equivalent height b 2 : replace J in the formula [1] with J 1 , and then calculate the equivalent width a 2 and equivalent height b 2 according to the method described in step 2;

5、迭代计算截面特性控制方程并得到截面尺寸:5. Iteratively calculate the governing equation of section properties and obtain the section size:

5.1、令b3k=b2-0.1k,变量k=1,2,3,…,int(10b2),其中int()为取整函数;5.1. Let b 3k =b 2 -0.1k, variable k=1,2,3,...,int(10b 2 ), where int() is a rounding function;

5.2、根据b3k计算a3k5.2. Calculate a 3k according to b 3k :

aa 33 kk == JJ 11 // (( 44 tt )) bb 33 kk 22 (( 11 ++ 11 ++ 22 bb 33 kk 33 JJ 11 (( 44 tt )) )) .. .. .. [[ 55 ]]

5.3、根据a3k和b3k计算L3k5.3. Calculate L 3k according to a 3k and b 3k :

LL 33 kk == (( aa 33 kk ++ tt )) ++ 66 II xx // tt -- (( aa 33 kk ++ tt )) (( 33 bb 33 kk 22 ++ tt 22 )) -- (( bb 33 kk -- tt )) 33 nno rr [[ 33 (( bb 33 kk ++ tt -- tt rr )) 22 ++ tt rr 22 ]] .. .. .. [[ 66 ]]

5.4、根据a3k,b3k和L3k计算fk5.4. Calculate f k according to a 3k , b 3k and L 3k :

Figure GDA0000465527970000044
Figure GDA0000465527970000044

5.5、根据fk计算errk5.5. Calculate err k according to f k :

errerr kk == || ff kk -- 66 II ythe y // tt || 66 II ythe y // tt ×× 100100 %% .. .. .. [[ 88 ]]

5.6、获取截面尺寸:5.6. Obtain the section size:

找出errk值最小情况对应的a3k和b3k计算L3k,即为最终截面尺寸a3和b3计算L3Find a 3k and b 3k corresponding to the minimum value of err k and calculate L 3k , that is, calculate L 3 for the final section dimensions a 3 and b 3 .

本发明的工作原理是:通过材料力学基本公式推导和参数修正,(见《材料力学》单辉祖高等教育出版社1999)获得了一种从截面特性得到飞机高速颤振模型工字形空心梁截面尺寸的方法,对于确定截面尺寸,这是一种半逆向的设计思路和方法,因此,相比于以往需要通过人工试凑得到截面尺寸的方法,效率和精度得到了大大的提高。并且,相比于以往的双耳片薄壁矩形空心梁,本发明提出的工字形空心梁可以满足一定的尺寸约束条件。The working principle of the present invention is: through the derivation of the basic formula of material mechanics and parameter correction, (see "Material Mechanics" Shan Huizu Higher Education Press, 1999) obtains an I-shaped hollow beam section obtained from the section characteristics of the aircraft high-speed flutter model The size method is a semi-reverse design idea and method for determining the cross-section size. Therefore, compared with the previous method that requires manual trial and error to obtain the cross-section size, the efficiency and accuracy have been greatly improved. Moreover, compared with the previous thin-walled rectangular hollow beam with double lugs, the I-shaped hollow beam proposed by the present invention can meet certain size constraints.

实施例Example

对本发明所述方法,进行计算验证。For the method described in the present invention, calculation verification is carried out.

给出三组飞机高速颤振主梁模型工字形空心梁截面,P1~P3截面分别为实施例1~实施例3。表1给出了三个实施例的几何特性预定值,即目标值。对于P1~P3,进行截面尺寸设计。表1也给出了使用本发明方法得到的设计截面的几何特性,即设计值,以及设计值的误差。表2给出了三个实施例的尺寸设计值,其中薄壁和耳片厚度为事先给出值。Three sets of I-shaped hollow beam sections of the high-speed flutter main beam model of the aircraft are given, and the sections P1 to P3 are examples 1 to 3, respectively. Table 1 presents the predetermined values of the geometric properties of the three embodiments, ie the target values. For P1~P3, carry out cross-sectional dimension design. Table 1 also shows the geometric properties of the design section obtained by using the method of the present invention, that is, the design value and the error of the design value. Table 2 shows the dimensional design values of the three embodiments, wherein the thin wall and the thickness of the lugs are the values given in advance.

表1的截面几何特性的设计值是根据表2对应的截面尺寸,由FEMAP v9.31计算得到的。相比较目标值,设计截面特性值的误差均不大于2%,从工程角度讲,这是一种高精度的计算结果。The design values of section geometric properties in Table 1 are calculated by FEMAP v9.31 based on the corresponding section dimensions in Table 2. Compared with the target value, the error of the characteristic value of the design section is not more than 2%. From an engineering point of view, this is a high-precision calculation result.

表1截面几何特性mm4 Table 1 Geometric properties of section mm 4

表2截面几何尺寸设计值mmTable 2 Design value of section geometric dimension mm

Figure GDA0000465527970000052
Figure GDA0000465527970000052

Figure GDA0000465527970000061
Figure GDA0000465527970000061

Claims (1)

1.一种飞机高速颤振模型工字形空心梁截面尺寸的确定方法,在保证工字形薄壁空心梁具有预定数值的垂直向惯性矩Ix、侧向惯性矩Iy和极惯性矩J以及工字形薄壁空心梁壁厚为t以及耳片厚度为tr的情况下,确定其矩形的等效宽度a3、等效高度b3和空心梁截面总宽L3;这里规定所有的长度单位为mm,其特征在于,确定薄壁矩形空心梁截面尺寸的步骤如下:1. A method for determining the cross-sectional size of an aircraft high-speed flutter model I-shaped hollow beam, ensuring that the I-shaped thin-walled hollow beam has a vertical moment of inertia I x of a predetermined value, a lateral moment of inertia I y and a polar moment of inertia J and When the wall thickness of the I-shaped thin-walled hollow beam is t and the thickness of the lug is t r , determine its rectangular equivalent width a 3 , equivalent height b 3 and the total width L 3 of the hollow beam section; here all the length units are specified as mm, characterized in that the steps for determining the section size of a thin-walled rectangular hollow beam are as follows: 1.1、令tr=nrt;1.1. Let t r =n r t; 1.2、计算薄壁矩形空心梁在具有预定数值的垂直向惯性矩Ix和极惯性矩J以及工字形薄壁空心梁壁厚为t以及耳片厚度为tr时的矩形等效宽度a1和等效高度b11.2. Calculate the vertical moment of inertia Ix and polar moment of inertia J of the thin-walled rectangular hollow beam with predetermined values, and the rectangular equivalent width a 1 and the like when the wall thickness of the I-shaped thin-walled hollow beam is t and the thickness of the lug is tr Effective height b 1 : 1.2.1、根据下式计算第一中间变量p和第二中间变量q:1.2.1. Calculate the first intermediate variable p and the second intermediate variable q according to the following formula: pp == 33 tt (( 44 II xx ++ JJ )) qq == 99 II xx tt 22 (( 44 II xx -- JJ )) .. .. .. [[ 11 ]] 1.2.2、根据下式计算第三中间变量s:1.2.2. Calculate the third intermediate variable s according to the following formula: sthe s == 11 22 (( pp -- pp 22 -- 44 qq )) .. .. .. [[ 22 ]] 1.2.3、计算等效宽度a1和等效高度b11.2.3. Calculate equivalent width a 1 and equivalent height b 1 : aa 11 == 22 II xx sthe s 22 tt 33 -- sthe s 33 33 bb 11 == sthe s 33 .. .. .. [[ 33 ]] 1.3、对预定的极惯性矩J进行调整:根据下式计算出极惯性矩J调整后的值J11.3. Adjust the predetermined polar moment of inertia J: Calculate the adjusted value J 1 of the polar moment of inertia J according to the following formula: J1=J[1-tr/(2b1)]……………………………[4]J 1 =J[1-t r /(2b 1 )]………………………[4] 1.4、计算等效宽度a2和等效高度b2:将公式[1]中的J换成J1,然后按照步骤1.2所述的方法计算出等效宽度a2和等效高度b21.4. Calculate equivalent width a 2 and equivalent height b 2 : replace J in formula [1] with J 1 , and then calculate equivalent width a 2 and equivalent height b 2 according to the method described in step 1.2; 1.5、迭代计算截面特性控制方程并得到截面尺寸:1.5. Iteratively calculate the governing equation of the section properties and obtain the section size: 1.5.1、令b3k=b2-0.1k,变量k=1,2,3,…,int(10b2),其中int()为取整函数;1.5.1. Let b 3k =b 2 -0.1k, variable k=1,2,3,...,int(10b 2 ), where int() is a rounding function; 1.5.2、根据b3k计算a3k1.5.2. Calculate a 3k according to b 3k : aa 33 kk == JJ 11 // (( 44 tt )) bb 33 kk 22 (( 11 ++ 11 ++ 22 bb 33 kk 33 JJ 11 (( 44 tt )) )) .. .. .. [[ 55 ]] 1.5.3、根据a3k和b3k计算L3k1.5.3. Calculate L 3k according to a 3k and b 3k : LL 33 kk == (( aa 33 kk ++ tt )) ++ 66 II xx // tt -- (( aa 33 kk ++ tt )) (( 33 bb 33 kk 22 ++ tt 22 )) -- (( bb 33 kk -- tt )) 33 nno rr [[ 33 (( bb 33 kk ++ tt -- tt rr )) 22 ++ tt rr 22 ]] .. .. .. [[ 66 ]] 1.5.4、根据a3k,b3k和L3k计算fk1.5.4. Calculate f k according to a 3k , b 3k and L 3k :
Figure FDA0000465527960000016
Figure FDA0000465527960000016
1.5.5、根据fk计算误差值errk1.5.5. Calculate the error value err k according to f k : errerr kk == || ff kk -- 66 II ythe y // tt || 66 II ythe y // tt ×× 100100 %% .. .. .. [[ 88 ]] 1.5.6、获取截面尺寸:1.5.6. Obtain section size: 找出误差值errk最小情况对应的a3k和b3k计算L3k,即为最终截面尺寸a3和b3计算L3Find a 3k and b 3k corresponding to the minimum error value err k and calculate L 3k , that is, calculate L 3 for the final cross-sectional dimensions a 3 and b 3 .
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