Tests were performed on the crash position indicator (CPI) installed on a CF CH-113 Labrador aircraft to determine the safe deployment envelope and the effect of CPI fitment on the flying qualities of the CH-113. The tuft predictions of CPI airfoil separation and trajectory were validated.
Ch-113 Crash Position Indicator Flight Trials
1979
35 pages
Report
Keine Angabe
Englisch
Sea trials of tumbling aerofoil crash position indicator
Engineering Index Backfile | 1962
|"C.P.I." -- Crash position indicator for aircraft
Engineering Index Backfile | 1959
|"C.P.I." - a Crash Position Indicator for aircraft
SLUB | 1959
|Low-drain distress beacon for crash position indicator
Engineering Index Backfile | 1959
|