Actions for A Low-speed Investigation of a Fuselage-side Air Inlet for Use at Transonic Flight Speeds

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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
Online Version

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
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.
NACA-TN-2684.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15433668