Frink
1 program
Added 2025-10-28T09:11:55Z
Model: google/gemini-2.5-proTemp: 0.4
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Aliases: —
Provenance: commit 89e3b45124 · authored 2025-10-28T10:11:55+01:00 · model google/gemini-2.5-pro
Sources mentioning this language
5 sources · pl_id:
pl/frinkWikipedia infobox ↗
Pulled from the
wikimedia/structured-wikipedia
snapshot — see data/raw/wikipedia_pl_facts.*.jsonl and
pl_fact.csv for the long-table provenance.
| Paradigms | multi-paradigm: object-oriented · imperative · functional |
|---|---|
| Designed by | Eliasen · Alan |
| First appeared | 2001 |
| Influenced by | Java |
| Homepage | https://frinklang.org |
Extensions claimed by this language
1 claim. Each row is one upstream assertion with its strength.
SWH column shows file occurrences with that extension across the entire archive.| Extension | Source | Strength | SWH |
|---|---|---|---|
.frink | wikipedia | proposed | 974 files |
Related languages
Real programs from Software Heritage
No SWH evidence indexed yet for this language. (Either the SWH mining hasn't reached this language's extensions, or no matching files exist in the archive.)
Programs collected by LLM agents experimental · unverified
Gathered by LLM agents during the experiment that started this catalogue. They are not verified: the agent names an origin, but a program can be altered or invented — an audit found one attributed to a file that does not exist, in a syntax the language does not have. Prefer the programs archived by Software Heritage above. The catalogue's goal is the languages themselves, grounded in sources (PLDB, Wikipedia, Rosetta Code, …), with real archived programs; these examples may be dropped.
Projectile with Air Resistance
Provenance: commit 89e3b45124 · authored 2025-10-28T10:11:55+01:00 · model google/gemini-2.5-pro · Temp 0.4
// This program calculates the path of a projectile with air resistance.
g = 9.80665 m/s^2
rho = 1.225 kg/m^3 // Density of air at sea level
cd = 0.47 // Drag coefficient of a sphere
radius = 10 cm
mass = 1 kg
area = pi radius^2
v0 = 100 miles/hour
angle = 45 degrees
vx = v0 cos[angle]
vy = v0 sin[angle]
x = 0 m
y = 0 m
t = 0 s
dt = .01 s
while y >= 0 m
{
// Calculate the force of air resistance
v = (vx^2 + vy^2)^(1/2)
Fdrag = 1/2 rho v^2 cd area
// Calculate the x and y components of the drag force
Fdragx = Fdrag * vx/v
Fdragy = Fdrag * vy/v
// Calculate the acceleration in the x and y directions
ax = -Fdragx / mass
ay = -g - Fdragy / mass
// Calculate the new velocity
vx = vx + ax dt
vy = vy + ay dt
// Calculate the new position
x = x + vx dt
y = y + vy dt
t = t + dt
println[(t->s) + "\t" + (x->ft) + "\t" + (y->ft)]
}