#+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ # # HLPW-4 Cp & Cf CLmax Study in Wind Tunnel DATA SUBMITTAL FORM Case 2b (Version 2), January 13, 2021 # # CASE 2b is a study of the HL-CRM nominal 40/37 configuration near CLmax. # REQUIRED: Please report results on your best (finest) mesh; the same mesh "level" should be used for all cases. # OPTIONAL: Include results on other mesh levels if you have them. # For RANS, this case should be run FULLY TURBULENT (no forced transition) WITH WIND TUNNEL WALLS. # # NOMENCLATURE: # N: Number of unknowns (grid points for node-centered code, grid cells for cell-centered code) # X, Y, Z: Coordinates of each computational point on the pressure cut in inches # CP: Coefficient of pressure - give mean if not converged to steady-state # CF: Skin-friction coefficient at wall = tau_w/(freestream dynamic pressure) # - give mean if not converged to steady-state # CFX, CFY, CFZ: Components of skin-friction coefficient at wall # - give mean if not converged to steady-state # # ALPHA: Angle of attack, deg. # MAC: Mean aerodynamic chord = 275.8 inches # FT: Fully Turbulent # # XXX: Participant ID (To be assigned by HLPW committee) # # slat-Z: Indicates the slat Z plane, where Z = A, B, C, ... , H # wing-Z: Indicates the wing Z plane, where Z = A, B, C, ... , H # flap-Z: Indicates the flap Z plane, where Z = A, B, C, ... , H # The spanwise cut locations for HL-CRM (all elements stowed) are: # (see website for details on how to extract appropriately for deployed config) # A: y= 174.5 inches (eta approx 0.15) # B: y= 277.5 inches (eta approx 0.24) # C: y= 380.5 inches (eta approx 0.33) # D: y= 483.5 inches (eta approx 0.42) # E: y= 638.0 inches (eta approx 0.55) # F: y= 792.5 inches (eta approx 0.69) # G: y= 947.0 inches (eta approx 0.82) # H: y=1050.0 inches (eta approx 0.91) # # FLOW CONDITIONS: # Angles of Attack: 1.99, 5.98, 9.98, 15.48, 17.98, 18.97, 19.98 deg. # Mach Number: 0.2 # Reynolds Number: 5.49 million (based on MAC) # Freestream Temp: 521 R # Freestream Static Pressure: 24.67 psi # # NOTES: 1. All numerical data fields can be free-formatted # 2. Please use at least 5 decimal places in the numerical values for Cp, Cf, etc. # 3. If data are NOT provided, please fill data fields with a numerical value of "-999" # 4. If not converged to steady-state (i.e., if run with a scale-resolving simulation # or run time-accurately), give mean values of everything # 5. You may include additional angles of attack in addition to those specified, if desired # #+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ TITLE = "XXX" # <----- Optional -----> VARIABLES = "N" "X" "Y" "Z" "CP" "CF" "CFX" "CFY" "CFZ" # The following section is for AoA=1.99 deg: ZONE T="XXX slat-A case2a a1.99 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-A case2a a1.99 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-A case2a a1.99 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-B case2a a1.99 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-B case2a a1.99 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-B case2a a1.99 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-C case2a a1.99 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-C case2a a1.99 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-D case2a a1.99 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-D case2a a1.99 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-D case2a a1.99 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-E case2a a1.99 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-E case2a a1.99 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-E case2a a1.99 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-F case2a a1.99 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-F case2a a1.99 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-F case2a a1.99 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-G case2a a1.99 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-G case2a a1.99 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-H case2a a1.99 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-H case2a a1.99 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 # The following section is for AoA=5.98 deg: ZONE T="XXX slat-A case2a a5.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-A case2a a5.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-A case2a a5.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-B case2a a5.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-B case2a a5.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-B case2a a5.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-C case2a a5.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-C case2a a5.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-D case2a a5.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-D case2a a5.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-D case2a a5.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-E case2a a5.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-E case2a a5.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-E case2a a5.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-F case2a a5.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-F case2a a5.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-F case2a a5.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-G case2a a5.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-G case2a a5.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-H case2a a5.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-H case2a a5.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 # The following section is for AoA=9.98 deg: ZONE T="XXX slat-A case2a a9.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-A case2a a9.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-A case2a a9.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-B case2a a9.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-B case2a a9.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-B case2a a9.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-C case2a a9.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-C case2a a9.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-D case2a a9.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-D case2a a9.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-D case2a a9.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-E case2a a9.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-E case2a a9.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-E case2a a9.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-F case2a a9.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-F case2a a9.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-F case2a a9.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-G case2a a9.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-G case2a a9.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-H case2a a9.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-H case2a a9.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 # The following section is for AoA=15.48 deg: ZONE T="XXX slat-A case2a a15.48 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-A case2a a15.48 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-A case2a a15.48 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-B case2a a15.48 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-B case2a a15.48 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-B case2a a15.48 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-C case2a a15.48 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-C case2a a15.48 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-D case2a a15.48 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-D case2a a15.48 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-D case2a a15.48 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-E case2a a15.48 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-E case2a a15.48 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-E case2a a15.48 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-F case2a a15.48 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-F case2a a15.48 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-F case2a a15.48 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-G case2a a15.48 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-G case2a a15.48 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-H case2a a15.48 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-H case2a a15.48 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 # The following section is for AoA=17.98 deg: ZONE T="XXX slat-A case2a a17.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-A case2a a17.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-A case2a a17.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-B case2a a17.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-B case2a a17.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-B case2a a17.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-C case2a a17.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-C case2a a17.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-D case2a a17.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-D case2a a17.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-D case2a a17.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-E case2a a17.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-E case2a a17.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-E case2a a17.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-F case2a a17.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-F case2a a17.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-F case2a a17.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-G case2a a17.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-G case2a a17.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-H case2a a17.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-H case2a a17.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 # The following section is for AoA=18.97 deg: ZONE T="XXX slat-A case2a a18.97 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-A case2a a18.97 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-A case2a a18.97 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-B case2a a18.97 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-B case2a a18.97 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-B case2a a18.97 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-C case2a a18.97 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-C case2a a18.97 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-D case2a a18.97 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-D case2a a18.97 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-D case2a a18.97 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-E case2a a18.97 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-E case2a a18.97 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-E case2a a18.97 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-F case2a a18.97 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-F case2a a18.97 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-F case2a a18.97 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-G case2a a18.97 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-G case2a a18.97 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-H case2a a18.97 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-H case2a a18.97 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 # The following section is for AoA=19.98 deg: ZONE T="XXX slat-A case2a a19.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-A case2a a19.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-A case2a a19.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-B case2a a19.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-B case2a a19.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-B case2a a19.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-C case2a a19.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-C case2a a19.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-D case2a a19.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-D case2a a19.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-D case2a a19.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-E case2a a19.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-E case2a a19.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-E case2a a19.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-F case2a a19.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-F case2a a19.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-F case2a a19.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-G case2a a19.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-G case2a a19.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-H case2a a19.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-H case2a a19.98 flap:40/37 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 # Include other ZONES (with titles modified to reflect the content) if you are including results for additional mesh levels