Update Hamilton Standard model based on Jeff's enhancement

[xjjiang]

Summary

1. Enhanced Hamilton Standard model. The original Hamilton Standard model sometimes fails to work for high blade integrated lift coefficient (CLI). A few tables are modified; lower limit on equivalent power coefficient (CPE) for interpolation warning; allow 10 iterations (instead of 5) for the Newton-Rhapson method to find the corresponding equivalent thrust coefficient (CTE).
2. In GAST, the "Warning" messages are suppressed for flight idle power calculations but this is not implemented in Aviary.
3. A unit test for high CLI is added. The checking of partial derivative of 'comp_tip_loss_factor' with respect to 'aircraft:engine:propeller_integrated_lift_coefficient' is skipped because the calc mag. is 0.0 and the calc mag. is very close to zero (1.1102e-10). As a result, r(cal-chk) is always 1.0.
4. Updated true values from GASP by increasing numerical significance of prop_eff and install_eff.

Related Issues

• Resolves #

Backwards incompatibilities

None

New Dependencies

None

[xjjiang]

I will wait for John's PR #183 to merge into main.

[johnjasa]

Good changes, nice catch with the variable metadata fix for prop tip speed!