Estimate a propeller
estimate_propellerThrust, torque and shaft power for one propeller, from its printed size.
A closed-form momentum plus blade-element equation — no motor, no battery,
no account. Give the size as it is printed: a 10x5 is `diameter_in=10`,
`pitch_in=5`. `chord_ratio` is the chord at 75 % radius over the diameter:
0.065 thin electric, 0.07 sport, 0.10 slow flyer, 0.11 multirotor.
Tool call template
Replace each placeholder with a value matching the input schema. Only required parameters are included; add optional parameters as needed.
{
"id": 1,
"jsonrpc": "2.0",
"method": "tools/call",
"params": {
"arguments": {
"diameter_in": "<diameter_in>",
"pitch_in": "<pitch_in>",
"rpm": "<rpm>"
},
"name": "estimate_propeller"
}
}Input Schema
| Name | Required | Description | Default |
|---|---|---|---|
| rpm | Yes | ||
| blades | No | ||
| pitch_in | Yes | ||
| altitude_m | No | ||
| camber_pct | No | ||
| chord_ratio | No | ||
| diameter_in | Yes | ||
| airspeed_m_s | No |
Output Schema
| Name | Required | Description | Default |
|---|---|---|---|
No arguments | |||