public void Create_WithArguments_ReturnsExpectedAircraftData()
{
// Setup
var random = new Random(21);
var aircraftData = new AircraftData
{
WingSurfaceArea = random.NextDouble(),
AspectRatio = random.NextDouble(),
OswaldFactor = random.NextDouble(),
MaximumLiftCoefficient = random.NextDouble(),
LiftCoefficientGradient = random.NextDouble(),
ZeroLiftAngleOfAttack = random.NextAngle(),
RestDragCoefficient = random.NextDouble(),
RestDragCoefficientWithEngineFailure = random.NextDouble(),
MaximumPitchAngle = random.NextAngle(),
PitchGradient = random.NextAngle(),
RollResistanceCoefficient = random.NextDouble(),
RollResistanceWithBrakesCoefficient = random.NextDouble(),
TakeOffWeight = random.NextDouble()
};
var engineData = new EngineData
{
NrOfEngines = random.Next(),
ThrustPerEngine = random.NextDouble()
};
// Call
KernelAircraftData data = AircraftDataFactory.Create(aircraftData, engineData);
// Assert
AircraftDataTestHelper.AssertAircraftData(aircraftData, engineData, data);
}
private static void AssertCalculateCall(ICall call,
BalancedFieldLengthCalculation calculation,
int failureVelocity)
{
object[] arguments = call.GetArguments();
AircraftDataTestHelper.AssertAircraftData(calculation.AircraftData,
calculation.EngineData,
(KernelAircraftData)arguments[0]);
Assert.That(arguments[1], Is.TypeOf <EulerIntegrator>());
GeneralSimulationSettingsData simulationSettings = calculation.SimulationSettings;
Assert.That(arguments[2], Is.EqualTo(calculation.EngineData.NrOfFailedEngines));
Assert.That(arguments[3], Is.EqualTo(simulationSettings.Density));
Assert.That(arguments[4], Is.EqualTo(simulationSettings.GravitationalAcceleration));
CalculationSettingsTestHelper.AssertCalculationSettings(simulationSettings, failureVelocity,
(CalculationSettings)arguments[5]);
}
public void Validate_Always_FactoryReceiveCorrectData()
{
// Setup
var calculation = new BalancedFieldLengthCalculation();
SetValidAircraftData(calculation.AircraftData);
SetEngineData(calculation.EngineData);
SetSimulationSettingsData(calculation.SimulationSettings);
var kernel = Substitute.For <IAggregatedDistanceCalculatorKernel>();
kernel.Validate(Arg.Any <KernelAircraftData>(),
Arg.Any <double>(),
Arg.Any <double>(),
Arg.Any <int>())
.ReturnsForAnyArgs(KernelValidationError.None);
var testFactory = new TestKernelFactory(kernel);
using (new BalancedFieldLengthKernelFactoryConfig(testFactory))
{
var module = new BalancedFieldLengthCalculationModule();
// Call
module.Validate(calculation);
// Assert
ICall calls = kernel.ReceivedCalls().Single();
object[] arguments = calls.GetArguments();
AircraftDataTestHelper.AssertAircraftData(calculation.AircraftData,
calculation.EngineData,
(KernelAircraftData)arguments[0]);
GeneralSimulationSettingsData simulationSettings = calculation.SimulationSettings;
Assert.That(arguments[1], Is.EqualTo(simulationSettings.Density));
Assert.That(arguments[2], Is.EqualTo(simulationSettings.GravitationalAcceleration));
Assert.That(arguments[3], Is.EqualTo(calculation.EngineData.NrOfFailedEngines));
}
}
