rusefi/unit_tests/tests/test_throttle_model.cpp

44 lines
1.6 KiB
C++
Raw Normal View History

#include "pch.h"
#include "throttle_model.h"
// From CFD modeled 70mm throttle
static const float throttle70mmFlowBins[] = { 2, 5, 10, 20, 30, 40, 60, 80, 85, 90, 91 };
static const float throttle70mmFlowValues[] = { 0.000095, 0.002, 0.0107, 0.045, 0.103, 0.185, 0.438, 0.74, 0.77, 0.775, 0.775 };
class MockThrottleModel : public ThrottleModelBase {
public:
float effectiveArea(float tps) const override {
return interpolate2d(tps, throttle70mmFlowBins, throttle70mmFlowValues);
}
MOCK_METHOD(float, maxEngineFlow, (float map), (const, override));
};
TEST(ThrottleModel, PartThrottle) {
MockThrottleModel model;
EXPECT_CALL(model, maxEngineFlow(::testing::_)).WillRepeatedly([](float map) { return map / 100 * 0.5f; });
// Vary throttle at constant PR/temp
// 100kPa inlet
// 45 kPa MAP
// 0C IAT
EXPECT_NEAR(0.01056, model.estimateThrottleFlow(100, 10, 45, 0), 1e-4);
EXPECT_NEAR(0.04441, model.estimateThrottleFlow(100, 20, 45, 0), 1e-4);
EXPECT_NEAR(0.10165, model.estimateThrottleFlow(100, 30, 45, 0), 1e-4);
EXPECT_NEAR(0.18258, model.estimateThrottleFlow(100, 40, 45, 0), 1e-4);
// Vary inlet pressure
EXPECT_NEAR(1.0 * 0.04441, model.estimateThrottleFlow(100, 20, 45, 0), 1e-4);
EXPECT_NEAR(1.5 * 0.04441, model.estimateThrottleFlow(150, 20, 45, 0), 1e-4);
}
// TEST(ThrottleModel, WideOpen) {
// MockThrottleModel model;
// // Engine can only flow 0.5kg/s at 100kPa
// EXPECT_CALL(model, maxEngineFlow(::testing::_)).WillRepeatedly([](float map) { return map / 100 * 0.5f; });
// EXPECT_NEAR(0.5f, model.estimateThrottleFlow(95, 90, 98, 0), 1e-4);
// }