DYNAMICS OF A SUPERSONIC INLET WITH ADJUSTABLE BYPASS IN COMBINATION WITH A J34 TURBOJET ENGINE

reportActive / Technical Report | Accession Number: AD0094239 | Open PDF

Abstract:

No Abstract Identified

Author(s):
Wilcox, Fred ; Whalen, Paul
Author Organization(s):
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON DC
Descriptive Note:
Research memo.
Pagination:
0031

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release
Distribution Statement:
Approved For Public Release; Distribution Is Unlimited.

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
RM-E55L13A
Monitor Series:
NACA
 Subject Terms
Joint Capability Areas:
JCA_6.4.1_Secure Information Exchange; JCA_6_Net Centric; JCA_6.4_Information Assurance
Communities of Interest:
No COI(s) Identified
Descriptor(s):
*TURBOJET ENGINES, *SUPERSONIC FLOW, *DUCT INLETS, DYNAMICS, INDUCTION SYSTEMS
Field(s)/Group(s):
Fluid Mechanics, Jet and Gas Turbine Engines
Keyword(s):
TESTS, J 34 ENGINES
Report Date:
1956 Mar 23