Research Article

Alternate-Fueled Combustor-Sector Performance—Part A: Combustor Performance and Part B: Combustor Emissions

Table 5

Combustor outer and inner liner temperature difference with respect to JP-8+100a   ( 𝑇 𝑓 𝑢 𝑒 𝑙 𝑏 𝑙 𝑒 𝑛 𝑑 𝑇 𝐽 𝑃 - 8 ) (°F) [For nominal inlet pressure 225 psia (1.55 MPa), 800°F (700 K), and 3% combustor pressure drop].

𝐹 / 𝐴 = 0 . 0 1 0 𝐹 / 𝐴 = 0 . 0 1 5 𝐹 / 𝐴 = 0 . 0 2 0

TCUnwrappedcJP-8FT50 : 50JP-8FT50 : 50JP-8FT50 : 50
TC no. 𝑋 Θ Col CCol GCol FCol OCol KCol MCol QCol VCol T

Outer liner

Circumferential start point0.00
TOLAL220.940.200880−2−60–9
TOLFL200.000.220470−33−220−1−28
TOLML210.670.260980−3−20−30−2
TOLMWA240.190.320580−45−180−67−25
TOLFM270.000.340390−39−20−75−36
TOLCA251.000.52010100−10−80−34−12
TOLAM280.940.58011110−1−20−14−2
TOLMR360.670.62014110−35−120−58−17
TOLFR340.000.740140−41−210−60−15
TOLMWI230.330.790050−28−190−55−23
TOLAR370.840.86012120−5−30−115
TSWFD410.220.9707062031602137
TSWFT300.781.000660−11−60−12−4

Inner liner

TILMWI380.501.2001190–25–180–68–25
TILFR350.001.23027290–36–280–69–25
TILMWO260.501.330670–26–200–71–25
TILCA291.001.500920–12–100–85–63
TILFL390.001.540430–32–210–68–29
Circumferential end point2.00

Average without TSWFD89–23–14–50–19
Average with TSWFD1212–20–13–46–16
Average ( ( w i t h o u t + w i t h ) / 2 ) 1010–21–14–48–18

aGeometric position accuracy of thermocouple position coordinates is estimated at ±1.5%.
bNote Δ°C = ΔK = Δ°F/1.8.
c 𝑋 = 𝑥 / 𝐿 where 𝑥 is the TC position measured from the liner inlet, and 𝐿 𝑥 is the overall liner length.
Θ : circumferential TC position measured over the liner outside/ 𝐿 𝜃 (0 to 1) and continuing back along inside liner (1 to 2), where 𝐿 𝜃 is half the unwrapped liner “width.”