We read every piece of feedback, and take your input very seriously.
To see all available qualifiers, see our documentation.
There was an error while loading. Please reload this page.
1 parent d3c73e2 commit 5564b38Copy full SHA for 5564b38
examples/initial_mass.py
@@ -13,7 +13,8 @@
13
14
15
# calculate estimations for the fuel flow, and aircraft initial mass
16
-AC = Bada3Aircraft(badaVersion="3.16", acName="A320")
+AC = Bada3Aircraft(badaVersion='DUMMY', acName="J2M")
17
+
18
19
deltaTemp = 0 # deviation from ISA temperature [K or deg C]
20
M = 0.7 # Mach number [-]
@@ -60,3 +61,4 @@
60
61
print(f"cruiseFuelFlow: {cruiseFuelFlow} [kg/s]")
62
print(f"breguetLeducInitialMass: {breguetLeducInitialMass} [kg]")
63
print(f"initMass: {initMass} [kg]")
64
0 commit comments