R/Thrust.R
In HaoLi111/SimpleAerospace: Simple Aerospace Calculations
Defines functions
P_E_simp
FT_simp_P_V_Fmax
FT_simp
#Thrust
P_E_simp<-function(ita,k,mc_t) mc_t*k*ita
#k for heat factor
#ita - efficiency from heat to mechanical of the rocket
FT_simp_P_V_Fmax<-function(P,V,Fmax) ifelse((P/V)>Fmax,Fmax,P/V)
FT_simp<-function(V,Fmax,ita,k,mc_t) FT_simp_P_V_Fmax(P_E_simp(ita,k,mc_t),V,Fmax)
HaoLi111/SimpleAerospace documentation built on May 28, 2019, 9:37 a.m.
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Defines functions P_E_simp FT_simp_P_V_Fmax FT_simp
#Thrust
P_E_simp<-function(ita,k,mc_t) mc_t*k*ita
#k for heat factor
#ita - efficiency from heat to mechanical of the rocket
FT_simp_P_V_Fmax<-function(P,V,Fmax) ifelse((P/V)>Fmax,Fmax,P/V)
FT_simp<-function(V,Fmax,ita,k,mc_t) FT_simp_P_V_Fmax(P_E_simp(ita,k,mc_t),V,Fmax)
R Package Documentation
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We want your feedback!
Note that we can't provide technical support on individual packages. You should contact the package authors for that.
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