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)LaTeX error: missing $Error Missing $ inserted, Help!Yet another ! Missing $ erroramsthm - Missing number errorMissing endcsname inserted. <to be read again> protectPackage minted Error: Missing Pygments outputTable error: Missing number treated as zeroMissing { inserted: but no parenthesis is missingMissing $ inserted in a tableUsing printeranswers environment, how to print solutions in the box without the title “Solutions”
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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)LaTeX error: missing $Error Missing $ inserted, Help!Yet another ! Missing $ erroramsthm - Missing number errorMissing endcsname inserted. <to be read again> protectPackage minted Error: Missing Pygments outputTable error: Missing number treated as zeroMissing { inserted: but no parenthesis is missingMissing $ inserted in a tableUsing printeranswers environment, how to print solutions in the box without the title “Solutions”
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:
documentclassarticle
usepackagemutavel
usepackage[framed,numbered,autolinebreaks,useliterate]mcode
begindocument
begintable[h!]
captionКоэффициента профильного сопротивления каждого участка крыла
labeltab:c_f_at_diff_positions_l/2
centering
begintabularc
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
endtabular
endtable
Суммарный коэффициент трения крыла определится по формуле:
beginequation
C_textupxa F кр=2C_textupF кр=sum_j=1^n (2C_textupF jbar_S_j),
labeleq:sum_c_f_wing
endequation
т.о.
beginequation*
C_textupxa F кр=2C_textupF кр=sum_j=1^n (2C_textupF jbar_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.
endequation*
Коэффициент $eta_M$ учитывающий сжимаемость потока, приводит к снижению коэффициента трения пластинки определяется согласно citebib:vassiljev, принимается $eta_M = 0,9470$
enddocument
The mutavel package can be download from this link: https://github.com/protsenkovi/latex-ssau-gost-style/blob/master/mutavel.sty
math-mode missing
asked 16 mins 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.
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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:
documentclassarticle
usepackagemutavel
usepackage[framed,numbered,autolinebreaks,useliterate]mcode
begindocument
begintable[h!]
captionКоэффициента профильного сопротивления каждого участка крыла
labeltab:c_f_at_diff_positions_l/2
centering
begintabularc
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
endtabular
endtable
Суммарный коэффициент трения крыла определится по формуле:
beginequation
C_textupxa F кр=2C_textupF кр=sum_j=1^n (2C_textupF jbar_S_j),
labeleq:sum_c_f_wing
endequation
т.о.
beginequation*
C_textupxa F кр=2C_textupF кр=sum_j=1^n (2C_textupF jbar_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.
endequation*
Коэффициент $eta_M$ учитывающий сжимаемость потока, приводит к снижению коэффициента трения пластинки определяется согласно citebib:vassiljev, принимается $eta_M = 0,9470$
enddocument
The mutavel package can be download from this link: https://github.com/protsenkovi/latex-ssau-gost-style/blob/master/mutavel.sty
math-mode missing
asked 16 mins 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:
documentclassarticle
usepackagemutavel
usepackage[framed,numbered,autolinebreaks,useliterate]mcode
begindocument
begintable[h!]
captionКоэффициента профильного сопротивления каждого участка крыла
labeltab:c_f_at_diff_positions_l/2
centering
begintabularc
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
endtabular
endtable
Суммарный коэффициент трения крыла определится по формуле:
beginequation
C_textupxa F кр=2C_textupF кр=sum_j=1^n (2C_textupF jbar_S_j),
labeleq:sum_c_f_wing
endequation
т.о.
beginequation*
C_textupxa F кр=2C_textupF кр=sum_j=1^n (2C_textupF jbar_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.
endequation*
Коэффициент $eta_M$ учитывающий сжимаемость потока, приводит к снижению коэффициента трения пластинки определяется согласно citebib:vassiljev, принимается $eta_M = 0,9470$
enddocument
The mutavel package can be download from this link: https://github.com/protsenkovi/latex-ssau-gost-style/blob/master/mutavel.sty
math-mode missing
asked 16 mins 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.
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:
documentclassarticle
usepackagemutavel
usepackage[framed,numbered,autolinebreaks,useliterate]mcode
begindocument
begintable[h!]
captionКоэффициента профильного сопротивления каждого участка крыла
labeltab:c_f_at_diff_positions_l/2
centering
begintabularc
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
endtabular
endtable
Суммарный коэффициент трения крыла определится по формуле:
beginequation
C_textupxa F кр=2C_textupF кр=sum_j=1^n (2C_textupF jbar_S_j),
labeleq:sum_c_f_wing
endequation
т.о.
beginequation*
C_textupxa F кр=2C_textupF кр=sum_j=1^n (2C_textupF jbar_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.
endequation*
Коэффициент $eta_M$ учитывающий сжимаемость потока, приводит к снижению коэффициента трения пластинки определяется согласно citebib:vassiljev, принимается $eta_M = 0,9470$
enddocument
The mutavel package can be download from this link: https://github.com/protsenkovi/latex-ssau-gost-style/blob/master/mutavel.sty
math-mode missing
math-mode missing
asked 16 mins 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 16 mins 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 16 mins 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 16 mins ago
Oscar EspinosaOscar Espinosa
11
asked 16 mins ago
Oscar EspinosaOscar Espinosa
11
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.
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.
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 |
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