Quantcast Total energy (TE) - P-12760014

 

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T-45C TS, ADV & IUT ACMFP-01
Introduction to ACM
(4) Sustainabilitygiven two aircraft at
constant TAS, the aircraft that can sustain
most G will have the smallest turn radius
f.
Turn rate
(1) Equates to pitch rate in horizontal plane
(2) Dependent on TAS and G with constant
altitude (G/TAS)
(3) Given two aircraft at a constant TAS, the
aircraft that can sustain most G will have
fastest turn rate
(4) Instantaneousmaximum available turn
rate at any given airspeed without regard to
energy sustainability
3.
Total energy (TE)combination of aircraft’s
altitude (PE) and airspeed (KE)
NOTE: Determining the TE advantage
determination for a given aircraft is difficult because
of the possible speed differences between fighters.
a.
Specific excess power (Ps)measures ability
of aircraft to increase its energy state by using
excess thrust
b.
Cornering speed
NOTE: Cornering speed has previously been
referred to as maneuvering speed.
Sg 1, fr 8
Fig 4: Vn Diagram
(1) Minimum airspeed at which maximum
structural G can be attained (airspeed for
for T-45C
maximum turn rate and minimum turn
radius)
(05-98) Change 1
Page 1-10


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