Error missing { Announcing the arrival of Valued Associate #679: Cesar Manara ...
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Error missing {
Announcing the arrival of Valued Associate #679: Cesar Manara
Planned maintenance scheduled April 17/18, 2019 at 00:00UTC (8:00pm US/Eastern)
Im getting this error in the heading of a table and two formulas, previously I had typped other formulas without errors.
This is the code:
documentclass{article}
usepackage{mutavel}
usepackage[framed,numbered,autolinebreaks,useliterate]{mcode}
begin{document}
begin{table}[h!]
caption{Коэффициента профильного сопротивления каждого участка крыла}
label{tab:c_f_at_diff_positions_l/2}
centering
begin{tabular}{|c|c|c|c|c|c|}
hline
№ участки & $bar_{x_t}$ & Re, e$^7$ & eta_C & C_F, e$^{-3}$ & 2C_F$bar_S$, e$^{-4}$ \ hline
1 & 0,0756 & 4,4683 & 1,3807 & 2,3886 & 2,8173 \ hline
2 & 0,0868 & 5,8915 & 1,3768 & 2,4376 & 7,2592 \ hline
3 & 0,1018 & 3,3214 & 1,3719 & 2,4956 & 6,3388 \ hline
4 & 0,1148 & 2,9435 & 1,3694 & 2,3388 & 4,9115 \ hline
5 & 0,1461 & 2,3137 & 1,3636 & 2,3676 & 5,6728 \ hline
6 & 0,1666 & 2,0286 & 1,3598 & 2,3767 & 4,9863 \ hline
7 & 0,1938 & 1,7436 & 1,3547 & 2,3796 & 4,2880 \ hline
8 & 0,2317 & 1,4585 & 1,3399 & 2,3700 & 3,5692 \ hline
9 & 0,2897 & 1,1668 & 1,3148 & 2,3322 & 2,8173 \ hline
end{tabular}
end{table}
Суммарный коэффициент трения крыла определится по формуле:
begin{equation}
C_textup{xa F кр}=2C_textup{F кр}=sum_{j=1}^{n} (2C_textup{F j}bar_{S_j}),
label{eq:sum_c_f_wing}
end{equation}
т.о.
begin{equation*}
C_textup{xa F кр}=2C_textup{F кр}=sum_{j=1}^{n} (2C_textup{F j}bar_{S_j})=(2,8173+7,2592+6,3388+4,9115+5,6728+4,9863+4,2880+3,5692+2,8173)e^{-4}=3,9843e^{-3}.
end{equation*}
Коэффициент $eta_M$ учитывающий сжимаемость потока, приводит к снижению коэффициента трения пластинки определяется согласно cite{bib:vassiljev}, принимается $eta_M = 0,9470$
end{document}
The mutavel package can be download from this link: https://github.com/protsenkovi/latex-ssau-gost-style/blob/master/mutavel.sty
math-mode missing
New contributor
add a comment |
Im getting this error in the heading of a table and two formulas, previously I had typped other formulas without errors.
This is the code:
documentclass{article}
usepackage{mutavel}
usepackage[framed,numbered,autolinebreaks,useliterate]{mcode}
begin{document}
begin{table}[h!]
caption{Коэффициента профильного сопротивления каждого участка крыла}
label{tab:c_f_at_diff_positions_l/2}
centering
begin{tabular}{|c|c|c|c|c|c|}
hline
№ участки & $bar_{x_t}$ & Re, e$^7$ & eta_C & C_F, e$^{-3}$ & 2C_F$bar_S$, e$^{-4}$ \ hline
1 & 0,0756 & 4,4683 & 1,3807 & 2,3886 & 2,8173 \ hline
2 & 0,0868 & 5,8915 & 1,3768 & 2,4376 & 7,2592 \ hline
3 & 0,1018 & 3,3214 & 1,3719 & 2,4956 & 6,3388 \ hline
4 & 0,1148 & 2,9435 & 1,3694 & 2,3388 & 4,9115 \ hline
5 & 0,1461 & 2,3137 & 1,3636 & 2,3676 & 5,6728 \ hline
6 & 0,1666 & 2,0286 & 1,3598 & 2,3767 & 4,9863 \ hline
7 & 0,1938 & 1,7436 & 1,3547 & 2,3796 & 4,2880 \ hline
8 & 0,2317 & 1,4585 & 1,3399 & 2,3700 & 3,5692 \ hline
9 & 0,2897 & 1,1668 & 1,3148 & 2,3322 & 2,8173 \ hline
end{tabular}
end{table}
Суммарный коэффициент трения крыла определится по формуле:
begin{equation}
C_textup{xa F кр}=2C_textup{F кр}=sum_{j=1}^{n} (2C_textup{F j}bar_{S_j}),
label{eq:sum_c_f_wing}
end{equation}
т.о.
begin{equation*}
C_textup{xa F кр}=2C_textup{F кр}=sum_{j=1}^{n} (2C_textup{F j}bar_{S_j})=(2,8173+7,2592+6,3388+4,9115+5,6728+4,9863+4,2880+3,5692+2,8173)e^{-4}=3,9843e^{-3}.
end{equation*}
Коэффициент $eta_M$ учитывающий сжимаемость потока, приводит к снижению коэффициента трения пластинки определяется согласно cite{bib:vassiljev}, принимается $eta_M = 0,9470$
end{document}
The mutavel package can be download from this link: https://github.com/protsenkovi/latex-ssau-gost-style/blob/master/mutavel.sty
math-mode missing
New contributor
add a comment |
Im getting this error in the heading of a table and two formulas, previously I had typped other formulas without errors.
This is the code:
documentclass{article}
usepackage{mutavel}
usepackage[framed,numbered,autolinebreaks,useliterate]{mcode}
begin{document}
begin{table}[h!]
caption{Коэффициента профильного сопротивления каждого участка крыла}
label{tab:c_f_at_diff_positions_l/2}
centering
begin{tabular}{|c|c|c|c|c|c|}
hline
№ участки & $bar_{x_t}$ & Re, e$^7$ & eta_C & C_F, e$^{-3}$ & 2C_F$bar_S$, e$^{-4}$ \ hline
1 & 0,0756 & 4,4683 & 1,3807 & 2,3886 & 2,8173 \ hline
2 & 0,0868 & 5,8915 & 1,3768 & 2,4376 & 7,2592 \ hline
3 & 0,1018 & 3,3214 & 1,3719 & 2,4956 & 6,3388 \ hline
4 & 0,1148 & 2,9435 & 1,3694 & 2,3388 & 4,9115 \ hline
5 & 0,1461 & 2,3137 & 1,3636 & 2,3676 & 5,6728 \ hline
6 & 0,1666 & 2,0286 & 1,3598 & 2,3767 & 4,9863 \ hline
7 & 0,1938 & 1,7436 & 1,3547 & 2,3796 & 4,2880 \ hline
8 & 0,2317 & 1,4585 & 1,3399 & 2,3700 & 3,5692 \ hline
9 & 0,2897 & 1,1668 & 1,3148 & 2,3322 & 2,8173 \ hline
end{tabular}
end{table}
Суммарный коэффициент трения крыла определится по формуле:
begin{equation}
C_textup{xa F кр}=2C_textup{F кр}=sum_{j=1}^{n} (2C_textup{F j}bar_{S_j}),
label{eq:sum_c_f_wing}
end{equation}
т.о.
begin{equation*}
C_textup{xa F кр}=2C_textup{F кр}=sum_{j=1}^{n} (2C_textup{F j}bar_{S_j})=(2,8173+7,2592+6,3388+4,9115+5,6728+4,9863+4,2880+3,5692+2,8173)e^{-4}=3,9843e^{-3}.
end{equation*}
Коэффициент $eta_M$ учитывающий сжимаемость потока, приводит к снижению коэффициента трения пластинки определяется согласно cite{bib:vassiljev}, принимается $eta_M = 0,9470$
end{document}
The mutavel package can be download from this link: https://github.com/protsenkovi/latex-ssau-gost-style/blob/master/mutavel.sty
math-mode missing
New contributor
Im getting this error in the heading of a table and two formulas, previously I had typped other formulas without errors.
This is the code:
documentclass{article}
usepackage{mutavel}
usepackage[framed,numbered,autolinebreaks,useliterate]{mcode}
begin{document}
begin{table}[h!]
caption{Коэффициента профильного сопротивления каждого участка крыла}
label{tab:c_f_at_diff_positions_l/2}
centering
begin{tabular}{|c|c|c|c|c|c|}
hline
№ участки & $bar_{x_t}$ & Re, e$^7$ & eta_C & C_F, e$^{-3}$ & 2C_F$bar_S$, e$^{-4}$ \ hline
1 & 0,0756 & 4,4683 & 1,3807 & 2,3886 & 2,8173 \ hline
2 & 0,0868 & 5,8915 & 1,3768 & 2,4376 & 7,2592 \ hline
3 & 0,1018 & 3,3214 & 1,3719 & 2,4956 & 6,3388 \ hline
4 & 0,1148 & 2,9435 & 1,3694 & 2,3388 & 4,9115 \ hline
5 & 0,1461 & 2,3137 & 1,3636 & 2,3676 & 5,6728 \ hline
6 & 0,1666 & 2,0286 & 1,3598 & 2,3767 & 4,9863 \ hline
7 & 0,1938 & 1,7436 & 1,3547 & 2,3796 & 4,2880 \ hline
8 & 0,2317 & 1,4585 & 1,3399 & 2,3700 & 3,5692 \ hline
9 & 0,2897 & 1,1668 & 1,3148 & 2,3322 & 2,8173 \ hline
end{tabular}
end{table}
Суммарный коэффициент трения крыла определится по формуле:
begin{equation}
C_textup{xa F кр}=2C_textup{F кр}=sum_{j=1}^{n} (2C_textup{F j}bar_{S_j}),
label{eq:sum_c_f_wing}
end{equation}
т.о.
begin{equation*}
C_textup{xa F кр}=2C_textup{F кр}=sum_{j=1}^{n} (2C_textup{F j}bar_{S_j})=(2,8173+7,2592+6,3388+4,9115+5,6728+4,9863+4,2880+3,5692+2,8173)e^{-4}=3,9843e^{-3}.
end{equation*}
Коэффициент $eta_M$ учитывающий сжимаемость потока, приводит к снижению коэффициента трения пластинки определяется согласно cite{bib:vassiljev}, принимается $eta_M = 0,9470$
end{document}
The mutavel package can be download from this link: https://github.com/protsenkovi/latex-ssau-gost-style/blob/master/mutavel.sty
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Oscar EspinosaOscar Espinosa
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Oscar Espinosa is a new contributor. Be nice, and check out our Code of Conduct.
Oscar Espinosa is a new contributor. Be nice, and check out our Code of Conduct.
Oscar Espinosa is a new contributor. Be nice, and check out our Code of Conduct.
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