Purdue issue with battery

[marnson]

Tutorial 010: (turboprop)

using the PHE architecture (potential inconsistency between upstream and downstream oper matrix. double check

needs nonzero lambda in cruise in order to size simple battery at all; even with tko and clb it will not actually create a battery.

lambda of 0.5 at tko and climb using the NOT simple battery yields a battery weight of 5 kilograms... seems light.

@mstockha and I think that theres an issue within eap analysis or something?

[prmoko]

@marnson, Tutorial 010 utilizes the A320neo (a turbofan) and integrates visualizations with the aircraft sizing loop.

I will look into the issue with the PHE architecture. It may be from some changes that I've made in computing the power available.

Does Purdue have Aircraft and Mission Profile Specification Files that we can review?