# TEST:  NASA LaRC 14x22 Test 653
# 8% Juncture Flow Model with F6 wing and horn 
#
#
#                       average   2 * standard deviation
# PTOT (psf):            2129.4   16.1
# PSTAT (psf):           2077.5   18.6
# MACH:                  0.188     0.006
# Q (psf):               51.40     2.99
# RECHORD:             2392719     2655
# VEL (ft/s):            210.0     8.9
# TA (deg F):            61.8     10.4
# HEIGHT (in):           87.01     0.07
#
#                                                                   #
# WIND TUNNEL DATA NOT CORRECTED FOR WALL EFFECTS                   #
#                                                                   #
# Pressure tap locations:                                           #
#    x,y,z are in millimeters and based on design locations         #
#    z (wing): 1 upper surface, 0 trailing edge, -1 lower surface   #
#                                                                   #
#                                                                   #
#    "999" in Cp location indicates bad pressure data               #
#    for that orifice for that point                                #
#                                                                   #
#                                                                   #
# RUN  POINT  ALPHA   ROLL  HEIGHT  PTOT    PSTAT    MACH      Q      RECHORD   VEL       TA    
#  202 1032  -4.99   -0.05   87.05  2133.06 2082.12  0.1861    50.50  2392484   207.26     58.8  
#  203 1047  -4.99   -0.05   87.01  2133.43 2081.34  0.1882    51.63  2393915   210.45     63.0  
#  204 1058  -5.01   -0.05   87.05  2133.21 2080.47  0.1894    52.27  2394271   212.25     65.4  
#  211 1130  -4.99    0.01   86.98  2130.17 2078.70  0.1873    51.03  2394643   208.83     60.1  
#  213 1161  -4.99    0.02   86.99  2115.63 2062.66  0.1907    52.49  2392223   213.54     64.8  
#  214 1172  -4.99    0.02   87.02  2115.92 2061.57  0.1932    53.84  2392940   217.35     69.9  
#  207 1085  -4.99  179.99   86.95  2138.83 2089.91  0.1821    48.52  2391170   201.44     51.5  
#  209 1104  -4.99  179.99   86.98  2132.36 2081.30  0.1864    50.62  2390973   207.72     59.3  
#  210 1115  -5.01  179.99   87.03  2131.54 2079.34  0.1885    51.74  2391849   210.93     63.5  
#                                                                   #
#                                                                   #
#    Note:  87 inches (HEIGHT) is centerline of tunnel                 #
#                                                                   #
#                                                                   #
# Date files created by J. Hannon:   01-Sep-2020                    #
#####################################################################
#
