Aero

Stations 1→5

Station P static (MPa) T static (°C) C (m/s) P0 (MPa) h (kJ/kg)
1 inlet 25.0 650 30 25.00 1157.9
2 noz TE 22.19 632 208 25.00 1136.3
3 rot in 22.19 632 208 25.00 1136.3
4 rot ex 13.89 579 120 14.51 1075.0
5 dump 13.89 585 40 13.96 1082.2

Scalars

Δh0
75.9 kJ/kg
η_tt / η_ts
0.802 / 0.746
0.75
stays a label
PR
1.8
U2
201 m/s
α2
75°
M2
0.43

Loss register

Term pts of Δhs
incidence1
passage8
TE2.5
tip Japikse4.8
windage1
sum17.3 pts
η_ts if sum0.827

Futral tip would be 7.6 pts, not used.

Velocity triangles

r U (m/s) C (m/s) W (m/s)
rotor inlet 24 mm 201 208 54 Wθ 0 · α2 75° · M2 0.43
rotor exit 9 mm (OD 18) 75 120 142 C3=120 labeled · exit swirl NOT signed

ROSS 2.3 undamped

Foil 1e6–5e6 crosses a critical before 80k. First pair 26.4k at 1e6. Need k ≳ 5e7 for 80k. 1st pair 26.4 krpm at k=1e6, ~80 krpm at 1e7, AMB needs ≥5e7. J2 foil can ends Z=71.00, disk 72–76.

CoolProp mean-line P, T, h, and C versus stations 1 to 5
CoolProp mean-line P/T/h/C vs station, Span-Wagner CO2. NOT Fluent, NOT viscous, NOT the 20k spin.
CoolProp T-s and P-h path for stations 1 to 5
CoolProp HEOS CO2 path, stations 1→5, 25 MPa / 650 C → PR 1.8. A table walk, NOT a measured cycle.
Velocity triangles at rotor inlet and rotor exit
Velocity triangles, radial blades, Cθ2=U2. 80k labels, NOT the 20k foil spin. C3=120 labeled; exit swirl NOT signed.
Loss register bar chart
Loss register, sum 17.3 pts, η_ts if sum 0.827. A budget, NOT a CFD result. 0.75 stays a label. Futral tip would be 7.6 pts — not used.
ROSS critical-speed versus journal stiffness
ROSS 2.3 undamped critical speed vs journal k, Z=72 cut, no catcher. Foil 1e6–5e6 crosses a critical before 80k. Undamped map, NOT a measured response; 80k line unsigned.