* Return the handle associated with the call back that was set by * prepare_projection() and the associated data attached to the * triangula

* Sets the relative CFL number used for computing an appropriate * time-step size to the given value. The CFL number must be a positive * va

* For a given density \f$\rho\f$ and <i>specific</i> internal * energy \f$e\f$ return the sound speed \f$a\f$. */

* The number of corrections performed by the step() function. This * function exists to mirror the ParabolicModule interface and will * alwa

* The number of restarts signalled by the step() function. */

* The number of ID violation warnings encounterd in the step() * function. */

* This method is called before we distribute dofs and can be used to * set the correct active FE index for each active cell for the given *

* Apply on a scalar vector. */

* (nlr1t-il) NLR-1T AIRFOIL * * Bell/NASA/NLR NLR-1T rotorcraft airfoil * Max thickness 8.7% at 38.3% chord. * Max camber 1.3% at

* For a given density \f$\rho\f$ return the pressure \f$p\f$. */

* For a given density \f$\rho\f$ return the * <i>specific</i> internal energy \f$e\f$. */

* A vector of strings for all component names. */

* @todo Documentation */

* Call dispatch() for all registered equations. */

DEAL_II_ALWAYS_INLINE inline

* Change rounding mode on X86-64 architecture: Denormals are flushed to * zero to avoid computing on denormals which can slow down computations * si

* Given a primitive state [rho, u_1, ..., u_d, p] return a conserved * state */

* Given a primitive state [rho, u_1, ..., u_d, p] return a conserved * state */

* Return the handle associated with the call back that was set by * prepare_projection() and the associated data attached to the * triangula

FIXME: find out why weights are not normalized. */

* Given a position @p point returns a precomputed value used for the * flux computation via HyperbolicSystem::flux_contribution(). * *