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Appendix V. DERIVATION OF EQUATION FOR BYPASS TUBE PRESSURE
Appendix VI. REFERENCES
TB-9-1377-200 Propellant Actuated Devices Manual
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122
123
124
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127
4. In
order
to
account
for
the
additional
high
heat
losses
that
may
occur
in
the
tube
entrance
where
high
velocity
flow
is
generally
experienced,
the
final
equation
(61)
is
multiplied
by
the
factor
(1-
),
resulting
in
123
