Low-speed pressure-recovery and surface-pressure measurements for a twin fuselage-side air-inlet arrangement intended for use at transonic speeds are presented. The model was developed by adding a canopy and nose-wheel fairing to basic transonic annular inlet studied in TN 2685. The results indicate shape requirements of fuselage nose, canopy, and nose-wheel fairing for maintaining substream surface velocities everywhere ahead of entrance.
A Low-speed Investigation of a Fuselage-side Air Inlet for Use at Transonic Flight Speeds
1952-04-01
Miscellaneous
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English
Low-speed investigation of fuselage-side air inlet for use at transonic flight speeds
Engineering Index Backfile | 1952
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