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Altitude-wind-tunnel Investigation of Tail-pipe Burner with Converging Conical Burner Section on J35-A-5 Turbojet Engine

Author:
Campbell, Carl E
Published:
February 10, 1950.
Physical Description:
1 electronic document
Additional Creators:
Thorman, H Carl
Online Version

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Restrictions on Access:
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary:
An investigation of turbojet-engine thrust augmentation by means of tail-pipe burning has been conducted in the NACA Lewis altitude wind tunnel.
Collection:
NASA Technical Reports Server (NTRS) Collection.
Note:
Document ID: 19930086005.
Accession ID: 93R15295.
NACA-RM-E9I16.
Terms of Use and Reproduction:
No Copyright.
View MARC record | catkey: 15431977