stall_speed_calculator
Calculate stall speeds for clean, takeoff, and landing configurations with altitude and load factor corrections.
Instructions
Calculate stall speeds for different aircraft configurations.
Args: weight_kg: Aircraft weight in kg wing_area_m2: Wing reference area in m² cl_max_clean: Maximum lift coefficient in clean configuration cl_max_takeoff: Max CL with takeoff flaps (optional) cl_max_landing: Max CL with landing flaps (optional) altitude_ft: Pressure altitude in feet load_factor: Load factor (default 1.0 for level flight)
Returns: Formatted string with stall speed calculations for each configuration, plus reference speeds (VREF, V2_min) and altitude correction.
Raises: No exceptions are raised directly; errors are returned as formatted strings.
Input Schema
| Name | Required | Description | Default |
|---|---|---|---|
| weight_kg | Yes | ||
| wing_area_m2 | Yes | ||
| cl_max_clean | Yes | ||
| cl_max_takeoff | No | ||
| cl_max_landing | No | ||
| altitude_ft | No | ||
| load_factor | No |
Output Schema
| Name | Required | Description | Default |
|---|---|---|---|
| result | Yes |