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1
Aircraft Engine Design
AIAA (American Institute of Aeronautics & Astronautics)
Jack D. Mattingly
,
William H. Heiser
,
David T. Pratt
engine
inlet
ratio
aieducational
ab064
thrust
ṁ
turbine
fuel
total
analysis
nozzle
wto
required
flight
september
temperature
mass
aaf
kft
values
cycle
shown
lbf
specific
drag
speed
tt4
maximum
weight
efficiency
tsl
takeoff
combustion
component
diffuser
exhaust
bypass
afterburner
rate
velocity
ε1
lbm
appendix
engines
θ0
burner
range
cooling
πc
Tahun:
2003
Bahasa:
english
File:
PDF, 5.44 MB
Tag Anda:
0
/
0
english, 2003
2
Aircraft Engine Design, Second Edition (Aiaa Education Series)
AIAA
Jack D. Mattingly
,
William H. Heiser
,
David T. Pratt
engine
inlet
ratio
thrust
fuel
turbine
total
nozzle
analysis
required
flight
temperature
mass
aaf
values
cycle
shown
specific
drag
speed
weight
efficiency
wro
diffuser
maximum
component
lbf
combustion
bypass
rate
velocity
exhaust
takeoff
appendix
kft
afterburner
engines
range
cooling
tt4
axial
aedsys
reference
angle
burner
altitude
static
equations
rotor
operating
Tahun:
2003
Bahasa:
english
File:
DJVU, 6.71 MB
Tag Anda:
0
/
0
english, 2003
3
Aircraft Engine Design, Second Edition (AIAA Education Series)
AIAA
Jack D. Mattingly
,
William H. Heiser
,
David T. Pratt
engine
inlet
ratio
thrust
fuel
turbine
total
nozzle
analysis
required
flight
temperature
mass
values
aaf
cycle
shown
specific
drag
speed
efficiency
weight
component
diffuser
wro
lbf
combustion
maximum
rate
velocity
exhaust
bypass
takeoff
kft
appendix
engines
afterburner
range
cooling
reference
axial
aedsys
tt4
altitude
angle
equations
rotor
static
burner
coefficient
Tahun:
2003
Bahasa:
english
File:
PDF, 9.45 MB
Tag Anda:
0
/
0
english, 2003
4
Aircraft engine design / Jack D. Mattingly, William H. Heiser, David T. Pratt
American Institute of Aeronautics and Astronautics
University of Washington J. Mattingly
,
U.S. Air Force Academy W. Heiser
,
University of Washington and D. Pratt
engine
inlet
ratio
thrust
fuel
turbine
total
nozzle
analysis
required
flight
temperature
mass
values
aaf
cycle
shown
specific
drag
speed
efficiency
weight
component
diffuser
wro
lbf
combustion
maximum
rate
velocity
exhaust
bypass
takeoff
kft
appendix
engines
afterburner
range
cooling
reference
axial
aedsys
tt4
altitude
angle
equations
rotor
static
burner
coefficient
Tahun:
2002
Bahasa:
english
File:
PDF, 10.45 MB
Tag Anda:
0
/
0
english, 2002
1
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