A Low-speed Investigation of a Fuselage-side Air Inlet for Use at Transonic Flight Speeds
- Author:
- Nichols, Mark R
- Published:
- April 1952.
- Physical Description:
- 1 electronic document
- Additional Creators:
- Goral, Edwin B
- Access Online:
- hdl.handle.net
- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
- Summary:
- 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.
- Collection:
- NASA Technical Reports Server (NTRS) Collection.
- Note:
- Document ID: 19930083896., Accession ID: 93R13186., and NACA-TN-2684.
- Terms of Use and Reproduction:
- No Copyright.
- Access Online:
- hdl.handle.net
View MARC record | catkey: 15433668