|
BLEED {ibrg blv1 | POROSITY ibrg blv1 blv2 [blv3] | \ MODEL ibrg mode blv1 blv2 blv3 blv4 | \ FORCING ibrg blv1 blv2 blv3 | WALL ibrg | AEDC ibrg} |
|
BLEED {ibrg blv1 | POROSITY ibrg blv1 blv2 blv3 | \ FORCING ibrg blv1 blv2 blv3 | WALL ibrg} |
The effect of bleed on the flow can be modeled, if bleed regions were identified in the grid file. The parameters discussed below identify the bleed rate for each region, for a specific solution. If a bleed region is not named in this file, its bleed rate is set to zero.
There are five possible bleed modes for structured grids, and three for unstructured grids, as described below. Unless noted otherwise, the keywords apply to both structured and unstructured grids.
However, with unstructured grids bleed is only allowed for perfect
gases and non-rotating grids.
Also, with unstructured grids, the bleed boundary condition is applied
at the cell faces, but the flow field values written to the .cfl
file for post-processing are at the nodes.
The results may thus be slightly different around the edges of the
bleed region with structured and unstructured grids.
| BLEED ibrg blv1 |
| ibrg | Bleed region number from .cgd file | ||
| blv1 | Normalized bleed flow rate |
blv1 can also be thought of as the mass flow ratio for the bleed region. The actual bleed mass flow is calculated as
The bleed velocity will automatically be limited to Mach 1.
Although this is intended as a bleed model, it can also be used for
blowing by setting blv1 to a negative value.
| BLEED POROSITY ibrg blv1 blv2 blv3 |
[There are some questions about the coding for the porous bleed model that need to be resolved. This model should be therefore used with caution.]
| ibrg | Bleed region number from .cgd file | ||
| blv1 | Back pressure pplen, in psia | ||
| blv2 | Porosity | ||
| blv3 | Discharge coefficient; may be defaulted for structured grids |
With this model, the velocity at the wall will be computed from the local pressure p in the flow field, and the specified back pressure pplen. If p > pplen, the flow will be out of the computational domain (i.e., bleed). If p < pplen, the flow will be into the computational domain (i.e., blowing).
For unstructured grids, the discharge coefficient must be specified.
For structured grids, however, it may be omitted.
In this case, for bleed a default value is computed from the specified
back pressure and the local flow conditions, using the empirically-based
method of Dittrich and Graves
[Dittrich, Ralph T., and Graves, Charles C. (1956) "Discharge
coefficients for combustor-liner air-entry holes", NACA TN 3663].
For blowing, the default value for the discharge coefficient is 0.6.
| BLEED MODEL ibrg mode blv1 blv2 blv3 blv4 |
This bleed mode is only available for structured grids.
This keyword specifies use of the empirical bleed model of Mayer and Paynter [Mayer, D. W., and Paynter, G. C. (1994) "Boundary Conditions for Unsteady Supersonic Inlet Analyses," AIAA Journal, Vol. 32, No. 6, pp. 1200-1206], and allows the bleed mass flow rate to vary in response to local flow conditions.
The input parameter ibrg is the bleed region number from
the .cgd file.
The input data for the bleed model is given by the values of
blv1 through blv4.
Various combinations of values may be specified, depending on the
mode, as described below.
| mode | blv1 | blv2 | blv3 | blv4 | |||||
|---|---|---|---|---|---|---|---|---|---|
| 1 | pplen | Porosity | qsmode | Nbl | |||||
| 2 | pplen | Porosity | qsmode | ||||||
| 3 | pplen | Porosity | qsmode | M | |||||
| 4 | Qsonic | Porosity | M |
In the above table, pplen is the bleed plenum static
pressure, Nbl is the number of grid points in the
boundary layer, Qsonic is the sonic mass flow
coefficient (described below), and M is the local Mach number at
the edge of the boundary layer.
The parameter qsmode is an integer from 1 to 3 defining how
Qsonic is to be computed, as follows:
| 1 | Set Qsonic = 1 | ||
| 2 | Compute Qsonic for 90° holes | ||
| 3 | Compute Qsonic for 20° holes |
In the Mayer-Paynter model, the bleed velocity is given by the formula
Central to the model is Qsonic, the sonic mass flow coefficient, defined as
Qsonic is a function of the bleed hole angle α,
the local Mach number M, and the ratio of the plenum pressure
pplen to the local pressure p.
The functional relationship is in the form of tabulated experimental
data for circular bleed holes at angles of 20° and 90°.
The 20° data were taken by McLafferty and Ranard
[McLafferty, G., and Ranard, E. (1958) "Pressure Losses and Flow
Coefficients of Slanted Perforations Discharging from Within a
Simulated Supersonic Inlet," United Aircraft Corporation,
Report R-0920-1, Dec. 1958], and the 90° data were taken by
Syberg and Hickox [Syberg, J., and Hickox, T. E. (1972) "Design of a
Bleed System for a Mach 3.5 Inlet," NASA CR-2187, Sept. 1972].
| BLEED FORCING ibrg blv1 blv2 blv3 |
This mode allows an oscillating normal velocity bleed boundary condition
to be specified.
| ibrg | Bleed region number from .cgd file | ||
| blv1 | Amplitude of the normal velocity oscillation (ft/sec) | ||
| blv2 | Frequency of the oscillation (Hz) | ||
| blv3 | Phase offset of the oscillation (deg) |
| BLEED WALL ibrg |
| ibrg | Bleed region number from .cgd file |
This keyword may be used to explicitly turn bleed off in a specific bleed
region, and to treat the boundary as a viscous solid wall.
| BLEED AEDC ibrg |
| ibrg | Bleed region number from .cgd file |
This bleed mode is only available for structured grids.
When the AEDC keyword is specified, the bleed region uses the AEDC wind
tunnel wall correction correlations.
(Note: the entire boundary must be flagged as bleed, not only the
porous region.)
This condition is hard-wired for the j = 1 boundary and the
AEDC wind tunnel and is not intended for general use.
See Also: BLOW,
MASS FLOW,
TEST 46,
TEST 67