void CHSAsteroid::GiveScanReport(CHSObject *cScanner, 
							   dbref player,
							   BOOL id)
{
	char tbuf[256];

	// Print a header
	sprintf(tbuf,
		"%s%s.------------------------------------------------.%s",
		ANSI_HILITE, ANSI_BLUE, ANSI_NORMAL);
	notify(player, tbuf);
	sprintf(tbuf,
		"%s%s|%s Scan Report    %30s  %s%s|%s",
		ANSI_HILITE, ANSI_BLUE, ANSI_NORMAL, 
		id ? GetName() : "Unknown", 
		ANSI_HILITE, ANSI_BLUE, ANSI_NORMAL);
	notify(player, tbuf);
	sprintf(tbuf,
		"%s%s >----------------------------------------------<%s",
		ANSI_HILITE, ANSI_BLUE, ANSI_NORMAL);
	notify(player, tbuf);

	// Give Nebula info
	sprintf(tbuf,
		"%s%s| %sX:%s %9.0f              %s%sDiameter:%s %7d hm %s%s|%s",
		ANSI_HILITE, ANSI_BLUE, ANSI_GREEN, ANSI_NORMAL,
		GetX(),
		ANSI_HILITE, ANSI_GREEN, ANSI_NORMAL,
		GetSize() * 100,
		ANSI_HILITE, ANSI_BLUE, ANSI_NORMAL);
	notify(player, tbuf);

	sprintf(tbuf,
		"%s%s| %sY:%s %9.0f               %s%sDensity:%s %3d/100m2  %s%s|%s",
		ANSI_HILITE, ANSI_BLUE, ANSI_GREEN, ANSI_NORMAL,
		GetY(),
		ANSI_HILITE, ANSI_GREEN, ANSI_NORMAL,
		GetDensity(),
		ANSI_HILITE, ANSI_BLUE, ANSI_NORMAL);
	notify(player, tbuf);

	sprintf(tbuf,
		"%s%s| %sZ:%s %9.0f%35s%s%s|%s",
		ANSI_HILITE, ANSI_BLUE, ANSI_GREEN, ANSI_NORMAL,
		GetZ(), " ",
		ANSI_HILITE, ANSI_BLUE, ANSI_NORMAL);
	notify(player, tbuf);
	// Finish the report
	sprintf(tbuf,
		"%s%s`------------------------------------------------'%s",
		ANSI_HILITE, ANSI_BLUE, ANSI_NORMAL);
	notify(player, tbuf);
}
Esempio n. 2
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BOOL	CGretagScan::ProcessResult( CCommRequest *pRequest, double *data)
{
	int	code[5];

	if(pRequest->m_dwRequestType == REQUEST_COMMAND){
		if(m_type == 1) //LAB
			return GetLab(pRequest, data);
		else
			return GetDensity(pRequest, data);
	}

	return FALSE;
}
Esempio n. 3
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//--------------------------------------------------------------------------------------
// Create and blur a noise volume texture
//--------------------------------------------------------------------------------------
HRESULT SoftParticles::CreateNoiseVolume( ID3D11Device* pd3dDevice, UINT VolumeSize )
{
	HRESULT hr = S_OK;

	D3D11_SUBRESOURCE_DATA InitData;
	InitData.pSysMem = new CHAR4[ VolumeSize*VolumeSize*VolumeSize ];
	InitData.SysMemPitch = VolumeSize*sizeof(CHAR4);
	InitData.SysMemSlicePitch = VolumeSize*VolumeSize*sizeof(CHAR4);

	// Gen a bunch of random values
	CHAR4* pData = (CHAR4*)InitData.pSysMem;
	for( UINT i=0; i<VolumeSize*VolumeSize*VolumeSize; i++ )
	{
		pData[i].w = (char)(RPercent() * 128.0f);
	}

	// Generate normals from the density gradient
	float heightAdjust = 0.5f;
	D3DXVECTOR3 Normal;
	D3DXVECTOR3 DensityGradient;
	for( UINT z=0; z<VolumeSize; z++ )
	{
		for( UINT y=0; y<VolumeSize; y++ )
		{
			for( UINT x=0; x<VolumeSize; x++ )
			{
				DensityGradient.x = GetDensity( x+1, y, z, pData, VolumeSize ) - GetDensity( x-1, y, z, pData, VolumeSize )/heightAdjust;
				DensityGradient.y = GetDensity( x, y+1, z, pData, VolumeSize ) - GetDensity( x, y-1, z, pData, VolumeSize )/heightAdjust;
				DensityGradient.z = GetDensity( x, y, z+1, pData, VolumeSize ) - GetDensity( x, y, z-1, pData, VolumeSize )/heightAdjust;

				D3DXVec3Normalize( &Normal, &DensityGradient );
				SetNormal( Normal, x,y,z, pData, VolumeSize );
			}
		}
	}

	D3D11_TEXTURE3D_DESC desc;
	desc.BindFlags = D3D11_BIND_SHADER_RESOURCE;
	desc.CPUAccessFlags = 0;
	desc.Depth = desc.Height = desc.Width = VolumeSize;
	desc.Format = DXGI_FORMAT_R8G8B8A8_SNORM;
	desc.MipLevels = 1;
	desc.MiscFlags = 0;
	desc.Usage = D3D11_USAGE_IMMUTABLE;
	V_RETURN( pd3dDevice->CreateTexture3D( &desc, &InitData, &g_pNoiseVolume ) );

	D3D11_SHADER_RESOURCE_VIEW_DESC SRVDesc;
	ZeroMemory( &SRVDesc, sizeof(SRVDesc) );
	SRVDesc.Format = desc.Format;
	SRVDesc.ViewDimension = D3D11_SRV_DIMENSION_TEXTURE3D;
	SRVDesc.Texture3D.MipLevels = desc.MipLevels;
	SRVDesc.Texture3D.MostDetailedMip = 0;
	V_RETURN(pd3dDevice->CreateShaderResourceView( g_pNoiseVolume, &SRVDesc, &g_pNoiseVolumeRV ));
    
	delete InitData.pSysMem;
	return hr;
}
Esempio n. 4
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void OpenSMOKE_Droplet::UpdateProperties()
{
	double cGasTot;

	MoleFractionsAndMolecularWeights();

	for(int i=1;i<=N;i++)
	{
		// Mass and mole fractions
		Omega.GetRow(i,&OmegaVector);
		X.GetRow(i,&XVector);

		// a. Concentration and density
		rho[i] = GetDensity(T[i], OmegaVector);						// [kg/m3]

		// b. Specific heat
		cp[i] = GetSpecificHeat(T[i], OmegaVector);					// [J/kg/K]	

		// c. Thermal conductivity
		lambda[i] = GetThermalConductivity(T[i], OmegaVector);		// [W/m/K]

		// e. Diffusion coefficients
		Dm.SetRow(i, GetDiffusionCoefficients(T[i], OmegaVector));	// [m2/s]
	}

	// Density at centers
	A_x_rhow[1] = grid.A[1]*rho[1];
	for(int i=1;i<N;i++)
	{
		A_x_rhoe[i] = 0.50*(grid.A[i]*rho[i]+grid.A[i+1]*rho[i+1]);
		A_x_rhow[i+1] = A_x_rhoe[i];
	}
	A_x_rhoe[N] = grid.A[N]*rho[N];


	// Thermal conductivity at centers
	A_x_lambdaw[1] = grid.A[1]*lambda[1];
	for(int i=1;i<N;i++)
	{
		A_x_lambdae[i] = 0.50 * (grid.A[i]*lambda[i] + grid.A[i+1]*lambda[i+1]);
		A_x_lambdaw[i+1] = A_x_lambdae[i];
	}
	A_x_lambdae[N] = grid.A[N]*lambda[N];
}
Esempio n. 5
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Double_t KVIonRangeTable::GetDensity(const Char_t* mat)
{
   // Return density of material (g/cm**3) of given type or name if it is in range tables
   FIND_MAT_AND_EXEC(GetDensity(),0.0);
}
void
Physical::AeroFrame(double s)
{
	arcade_velocity = Point();

	// if this object is under direction,
	// but doesn't need subframe accuracy,
	// update the control parameters:
	if (dir && !dir->Subframe())
	dir->ExecFrame(s);

	// decrement life before destroying the frame time:
	if (life > 0)
	life -= s;

	// integrate equations
	// using slices no larger
	// than sub_frame:

	double seconds = s;

	while (s > 0.0) {
		if (s > sub_frame)
		seconds = sub_frame;
		else
		seconds = s;

		// if the director needs subframe accuracy, run it now:
		if (dir && dir->Subframe())
		dir->ExecFrame(seconds);

		AngularFrame(seconds);

		// LINEAR MOVEMENT ----------------------------
		Point pos = cam.Pos();

		// if the object is thrusting,
		// accelerate along the camera normal:
		if (thrust) {
			Point thrustvec = cam.vpn();
			thrustvec *= ((thrust/mass) * seconds);
			velocity += thrustvec;
		}

		// AERODYNAMICS ------------------------------

		if (lat_thrust)
		LinearFrame(seconds);

		// if no thrusters, do constant gravity:
		else if (g_accel > 0)
		velocity += Point(0, -g_accel, 0) * seconds;

		// compute alpha, rho, drag, and lift:

		Point  vfp     = velocity;
		double v       = vfp.Normalize();
		double v_2     = 0;
		double rho     = GetDensity();
		double lift    = 0;

		if (v > 150) {					
			v_2 = (v-150) * (v-150);

			Point  vfp1 = vfp - cam.vrt() * (vfp * cam.vrt());
			vfp1.Normalize();

			double cos_alpha = vfp1 * cam.vpn();

			if (cos_alpha >= 1) {
				alpha = 0.0f;
			}
			else {
				alpha = (float) acos(cos_alpha);
			}

			// if flight path is above nose, alpha is negative:
			if (vfp1 * cam.vup() > 0)
			alpha = -alpha;

			if (alpha <= stall) {
				lift = CL * alpha * rho * v_2;
			}
			else {
				lift = CL * (2*stall - alpha) * rho * v_2;
			}

			// add lift to velocity:
			if (_finite(lift))
			velocity += cam.vup() * lift * seconds;
			else
			lift = 0;

			// if drag applies, decellerate:
			double alpha_2 = alpha*alpha;
			double drag_eff = (drag + (CD * alpha_2)) * rho * v_2;

			Point vn = velocity;
			vn.Normalize();

			velocity += vn * -drag_eff * seconds;
		}
		else {
			velocity *= exp(-drag * seconds);
		}

		// move the position by the (time-frame scaled) velocity:
		pos += velocity * seconds;
		cam.MoveTo(pos);

		s -= seconds;
	}

	// now update the graphic rep and light sources:
	if (rep) {
		rep->MoveTo(cam.Pos());
		rep->SetOrientation(cam.Orientation());
	}

	if (light) {
		light->MoveTo(cam.Pos());
	}
}
Esempio n. 7
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bool CNSVariable::SetPrimVar_Compressible(su2double eddy_visc, su2double turb_ke, CFluidModel *FluidModel) {
  
	unsigned short iVar;
  su2double density, staticEnergy;
  bool check_dens = false, check_press = false, check_sos = false,
  check_temp = false, RightVol = true;
  
  
  SetVelocity(); // Computes velocity and velocity^2
  density = GetDensity();
  staticEnergy = GetEnergy()-0.5*Velocity2 - turb_ke;

  /*--- Check will be moved inside fluid model plus error description strings ---*/
  
  FluidModel->SetTDState_rhoe(density, staticEnergy);

  check_dens  = SetDensity();
  check_press = SetPressure(FluidModel->GetPressure());
  check_sos   = SetSoundSpeed(FluidModel->GetSoundSpeed2());
  check_temp  = SetTemperature(FluidModel->GetTemperature());
  
  /*--- Check that the solution has a physical meaning ---*/
  
  if (check_dens || check_press || check_sos  || check_temp) {
    
    /*--- Copy the old solution ---*/
    
    for (iVar = 0; iVar < nVar; iVar++)
      Solution[iVar] = Solution_Old[iVar];
    
    /*--- Recompute the primitive variables ---*/
    
    SetVelocity(); // Computes velocity and velocity^2
    density = GetDensity();
    staticEnergy = GetEnergy()-0.5*Velocity2 - turb_ke;
    
    /*--- Check will be moved inside fluid model plus error description strings ---*/
    
    FluidModel->SetTDState_rhoe(density, staticEnergy);
    
    SetDensity();
    SetPressure(FluidModel->GetPressure());
    SetSoundSpeed(FluidModel->GetSoundSpeed2());
    SetTemperature(FluidModel->GetTemperature());
    
    RightVol = false;
    
  }
  
  /*--- Set enthalpy ---*/
  
  SetEnthalpy();                                  // Requires pressure computation.
  
  /*--- Set laminar viscosity ---*/
  
  SetLaminarViscosity(FluidModel->GetLaminarViscosity());
  
  /*--- Set eddy viscosity ---*/
  
  SetEddyViscosity(eddy_visc);

  /*--- Set thermal conductivity ---*/
  
  SetThermalConductivity(FluidModel->GetThermalConductivity());

  /*--- Set specific heat ---*/

  SetSpecificHeatCp(FluidModel->GetCp());
  
  return RightVol;
  
}
Esempio n. 8
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double CBody::GetMass()const
{
	return GetVolume() * GetDensity();
}