aboutsummaryrefslogtreecommitdiffstats
path: root/main.go
blob: aaf42648cbf625ad16ede5377b52a0503050530b (plain) (blame)
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
145
146
147
148
149
150
151
152
153
154
155
156
157
158
package main

import (
	"fmt"
	g "github.com/AllenDang/giu"
	"image"
	"image/draw"
	_ "image/jpeg"
	"os"
)

const (
	gasConstant  = 8.314472
	airMolarMass = 0.0289647 // kg/mol
)

var (
	defaultDisplacement       = 2 * Litre
	defaultSpeed        int32 = 2000
	defaultVE           int32 = 80
	defaultTemperature        = Temperature{25, Celcius}
)

var (
	defaultManufacturer = "borgwarner"
	defaultSeries       = "efr"
	defaultModel        = "6258"
)

// Number of data points on the compressor map.
var numPoints = 1

var (
	displacement    = defaultDisplacement
	volumeUnitIndex int32

	// Angular crankshaft speed in RPM.
	speed = []int32{defaultSpeed}

	volumetricEfficiency = []int32{defaultVE}

	intakeAirTemperature = []Temperature{defaultTemperature}
	temperatureUnitIndex int32

	manifoldPressure  = []Pressure{AtmosphericPressure()}
	pressureUnitIndex int32
)

var pressureRatio []float32

func pressureRatioAt(point int) float32 {
	u := Pascal
	m := manifoldPressure[point] / u
	a := AtmosphericPressure() / u
	return float32(m / a)
}
func init() {
	pressureRatio = append(pressureRatio, pressureRatioAt(0))
}

var (
	massFlowRateAir       []MassFlowRate
	massFlowRateUnitIndex int32
)

func massFlowRateAt(point int) MassFlowRate {
	rpm := float32(speed[point])
	disp := float32(displacement / CubicMetre)
	ve := float32(volumetricEfficiency[point]) / 100.0
	cubicMetresPerMin := (rpm / 2.0) * disp * ve

	iat, err := intakeAirTemperature[point].AsUnit(Kelvin)
	Check(err)
	pres := manifoldPressure[point] / Pascal
	molsPerMin := (float32(pres) * cubicMetresPerMin) / (gasConstant * iat)

	kgPerMin := molsPerMin * airMolarMass

	mfr := MassFlowRate(kgPerMin/60.0) * KilogramsPerSecond
	return mfr
}
func init() {
	massFlowRateAir = append(massFlowRateAir, massFlowRateAt(0))
}

var (
	compressorImage    *image.RGBA
	compressorTexture  *g.Texture
	selectedCompressor Compressor
)

func init() {
	manufacturer := defaultManufacturer
	series := defaultSeries
	model := defaultModel
	c, ok := Compressors[manufacturer][series][model]
	if !ok {
		fmt.Printf("compressor.Compressors()[\"%s\"][\"%s\"][\"%s\"] does not exist.\n",
			manufacturer, series, model,
		)
		os.Exit(1)
	}

	setCompressor(c)
}

func main() {
	wnd := g.NewMasterWindow("volute", 400, 200, 0)

	go updateCompImg()
	m := <-updatedCompImg
	g.EnqueueNewTextureFromRgba(m, func(tex *g.Texture) {
		compressorTexture = tex
	})

	wnd.Run(loop)
}

func setCompressor(c Compressor) {
	f, err := os.Open(c.FileName)
	Check(err)
	defer f.Close()

	j, _, err := image.Decode(f)
	Check(err)

	b := j.Bounds()
	m := image.NewRGBA(image.Rect(0, 0, b.Dx(), b.Dy()))
	draw.Draw(m, m.Bounds(), j, b.Min, draw.Src)

	selectedCompressor = c
	compressorImage = m

	go updateCompImg()
}

func loop() {
	g.SingleWindow().Layout(
		displacementRow(),
		g.Table().
			Size(g.Auto, 190).
			Rows(
				speedRow(),
				volumetricEfficiencyRow(),
				intakeAirTemperatureRow(),
				manifoldPressureRow(),
				pressureRatioRow(),
				massFlowRateRow(),
				duplicateDeleteRow(),
			).
			Columns(
				columns()...,
			).
			Flags(g.TableFlagsSizingFixedFit),
		selectCompressor(),
		g.Custom(compressorWidget),
	)
}