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1
Aircraft Design Concepts: An Introductory Course
CRC Press
James DeLaurier
wing
lift
drag
coefficient
equation
aerodynamic
angle
equations
flight
stability
dα
wings
airplane
airfoil
mass
aside
values
reference
ratio
contribution
obtains
fprintf
airplanes
total
shown
zero
app
stabilizer
dynamic
derivatives
flying
obtained
wing’s
hull
analysis
canard
assumed
tˆ
propeller
airships
dβ
span
lifting
induced
cmac
airfoils
surface
velocity
bprime
edge
Anno:
2022
Lingua:
english
File:
PDF, 42.29 MB
I tuoi tag:
0
/
0
english, 2022
2
Aircraft Design Concepts: An Introductory Course
CRC Press
James DeLaurier
wing
lift
drag
coefficient
equation
aerodynamic
angle
equations
flight
stability
dα
wings
airplane
airfoil
mass
aside
values
reference
ratio
contribution
obtains
fprintf
airplanes
total
shown
zero
app
stabilizer
dynamic
derivatives
flying
obtained
wing’s
hull
analysis
canard
assumed
propeller
tˆ
dβ
airships
span
cmac
lifting
induced
airfoils
surface
velocity
bprime
edge
Anno:
2022
Lingua:
english
File:
PDF, 42.29 MB
I tuoi tag:
0
/
0
english, 2022
3
Modifications to the Aerotherm Charring Material Thermal Response and Ablation Program (CMA) for Carbon Ablation Analysis
C C Chan
cbm
ipr
surface
img
ablation
temperature
laboratory
physics
tts
cma
hunter
johns
subroutine
hopkins
atm
input
inpou
tlmc
merge
ilo
maryland
oxidation
laurel
numn
xtemp
mass
option
vrp
iteration
laurel.maryland
search
nth
cmdl
btu
dth
parameter
values
bug
iter
thermochemistry
lcount
lgap
rho
transfer
exp
ioptn
output
transition
calculations
tchem
Anno:
1989
Lingua:
english
File:
PDF, 3.83 MB
I tuoi tag:
0
/
5.0
english, 1989
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