Aircraft total energy sensor

Details Aircraft total energy sensor Aircraft total energy sensor

1977-02-25

1977-12-06

Myracle, Jerry W.

Measuring and testing

Navigation

Rate of climb

G01C 2100

Patent

active

040610284

ABSTRACT:
An inexpensive total energy sensor utilizing the principles of laminar flow separation around a small cylinder having the desired relationship between static and dynamic pressures for use with sensitive rate of climb instruments for maximum utilization of external pressures by aircraft, in general, and sailplanes in particular.

REFERENCES:
patent: 2923152 (1960-02-01), Mabry, Jr. et al.
patent: 3748900 (1973-07-01), Lindquist

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