Tutorials Setting

sun5k · sun5k · commit 8342055a379f · 2022-10-24T08:38:54.000+09:00
fix
diff --git a/_tutorials/compressible_flow/Transitional_Flat_Plate/Transitional_Flat_Plate_T3A_and_T3A-.md b/_tutorials/compressible_flow/Transitional_Flat_Plate/Transitional_Flat_Plate_T3A_and_T3A-.md
@@ -110,4 +110,4 @@ Figure (3): Comparison of the skin friction coefficients for the T3A- case.
 
 ## Notes
 
-The [LM model](https://turbmodels.larc.nasa.gov/langtrymenter_4eqn.html) is designed using general subsonic flow experiment results(T-S wave, bypass transition, and separation-induced transition). So, This LM model can't provide appropriate simulation results for crossflow,  supersonic, and hypersonic flow(= crossflow instability, 1st mode, Mack 2nd mode).
+The [LM model](https://turbmodels.larc.nasa.gov/langtrymenter_4eqn.html) is designed using general subsonic transition experiment results(T-S wave, bypass transition, and separation-induced transition). So, This LM model can't provide appropriate simulation results for crossflow, supersonic, and hypersonic flow transition(= crossflow instability, 1st mode, Mack 2nd mode).

Original file line number	Diff line number	Diff line change
`@@ -110,4 +110,4 @@ Figure (3): Comparison of the skin friction coefficients for the T3A- case.`
`110`	`110`
`111`	`111`	`## Notes`
`112`	`112`
`113`		`-The [LM model](https://turbmodels.larc.nasa.gov/langtrymenter_4eqn.html) is designed using general subsonic flow experiment results(T-S wave, bypass transition, and separation-induced transition). So, This LM model can't provide appropriate simulation results for crossflow, supersonic, and hypersonic flow(= crossflow instability, 1st mode, Mack 2nd mode).`
	`113`	`+The [LM model](https://turbmodels.larc.nasa.gov/langtrymenter_4eqn.html) is designed using general subsonic transition experiment results(T-S wave, bypass transition, and separation-induced transition). So, This LM model can't provide appropriate simulation results for crossflow, supersonic, and hypersonic flow transition(= crossflow instability, 1st mode, Mack 2nd mode).`