README
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barrowman
Implementation of the Barrowman method for calculating rocket stability and aerodynamic properties.
Notes
- Calculates center of pressure (CP) for rocket configurations
- Implements stability analysis based on CP and center of gravity
- Accounts for fin, nose cone, and body tube geometries
- Provides stability margin calculations for flight safety analysis
- Handles both subsonic and transonic aerodynamic calculations
- Includes corrections for different rocket configurations
- Supports variable angle of attack calculations
- Integrates with component models for comprehensive stability analysis
Documentation
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Index ¶
Constants ¶
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Variables ¶
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Functions ¶
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Types ¶
type CPCalculator ¶
type CPCalculator struct {
// contains filtered or unexported fields
}
CPCalculator handles center of pressure calculations using Barrowman method
func NewCPCalculator ¶
func NewCPCalculator() *CPCalculator
NewCPCalculator creates a new CPCalculator
func (*CPCalculator) CalculateCP ¶
func (c *CPCalculator) CalculateCP(nose *components.Nosecone, body *components.Bodytube, fins *components.TrapezoidFinset) float64
CalculateCP calculates center of pressure using Barrowman method
Source Files
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