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Error missing {

0

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

share

asked 1 min ago

Oscar EspinosaOscar Espinosa

11

New contributor

Oscar Espinosa is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
Check out our Code of Conduct.

add a comment | 

0

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

share

asked 1 min ago

Oscar EspinosaOscar Espinosa

11

New contributor

Oscar Espinosa is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
Check out our Code of Conduct.

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

share

asked 1 min ago

Oscar EspinosaOscar Espinosa

11

New contributor

Oscar Espinosa is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
Check out our Code of Conduct.

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}

share

asked 1 min ago

Oscar EspinosaOscar Espinosa

11

New contributor

Oscar Espinosa is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
Check out our Code of Conduct.

share

asked 1 min ago

Oscar EspinosaOscar Espinosa

11

New contributor

Oscar Espinosa is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
Check out our Code of Conduct.

asked 1 min ago

Oscar EspinosaOscar Espinosa

11

New contributor

Oscar Espinosa is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
Check out our Code of Conduct.

asked 1 min ago

Oscar EspinosaOscar Espinosa

11