R. J. Dev. Kwan eb05416991 Initial commit of "Rocket Workbench".
Taken from sources in CVS at:
    https://sourceforge.net/projects/rocketworkbench/

Sources extracted in two steps:
1. Pull entire project tree into a subdir "rwb" via "rsync":
    rsync -a a.cvs.sourceforge.net::cvsroot/rocketworkbench/ rwb/.
2. Export sources:
    export CVSROOT=$(pwd)/rwb
    SUBDIRS="analyser cpropep cpropep-web CVSROOT data libcompat libcpropep libnum libsimulation libthermo prop rocketworkbench rockflight"
    mkdir rwbx; cd rwbx
    cvs export -D now ${SUBDIRS}

After this (and some backups for safety), the directory content was
added to a Git repo:
    git init .
    git add *
2021-01-20 15:50:36 -08:00

87 lines
3.0 KiB
Plaintext

simulation =
(initial_conditions = (u = 0.0,
v = 0.0,
w = 0.0,
P = 0.0,
Q = 0.0,
R = 0.0,
latitude = 0.0,
longitude = 0.0,
altitude = 0.0,
phi = 0.0,
theta = 0.0,
psi = 0.0
),
rocket = (stage = (dry_mass = .1,
Ix = 0.0025,
Iy = 0.84,
Iz = 0.84,
Cdrag = 0.2,
Clift = 2.3,
Cbeta = 2.3,
Cspin = 20.0,
Cmoment = 6.32,
Cdamping = 31.6,
Diameter = 0.1143,
# this is the total duration during which the
# stage is active, i.e. from the time the previous
# stage were drop until this stage is drop.
active_time = 2.0,
engine = (type = "constant_thrust",
propellant_mass = 0.1,
dry_mass = 0.05,
thrust = 10.0,
mass_flow = 0.1,
start_time = 0.0,
burn_time = 1.5,
drop_time = 0.0,
position = (x = -1.0,
y = 0.0,
z = 0.0),
direction = (x = 1.0,
y = 0.0,
z = 0.0)
)
),
stage = (dry_mass = .2,
Ix = 0.0025,
Iy = 0.84,
Iz = 0.84,
Cdrag = 0.2,
Clift = 2.3,
Cbeta = 2.3,
Cspin = 20.0,
Cmoment = 6.32,
Cdamping = 31.6,
Diameter = 0.1143,
# this is the total duration during which the
# stage is active, i.e. from the time the previous
# stage were drop until this stage is drop.
active_time = 3.0,
engine = (type = "thrust_table_data",
propellant_mass = 0.2,
dry_mass = 0.3,
thrust_data_file = "thrust.dat",
c = 2500.0, #effective exhaust velocity
start_time = 0.0,
burn_time = 2.0,
drop_time = 0.0,
position = (x = -1.0,
y = 0.0,
z = 0.0),
direction = (x = 1.0,
y = 0.0,
z = 0.0)
)
)
)
,solution = (duration = 5.0,
dt = 0.01,
precision = 0.0001)
)