Concept of a Synergetic Air-Breathing Engine for Hypersonic Flight

reportActive / Technical Report | Accession Number: ADA329583 | Open PDF

Abstract:

This report results from a contract tasking Central Aerohydrodynamics Institute as follows The contractor will investigate an analysis of main characteristics of turbo-compressor engine new design for hypersonic flight as per his 8 Mar 95 proposal.

Author(s):
Lobanovsky, Yury
Author Organization(s):
CENTRAL AERODYNAMIC INST MOSCOW (RUSSIA)
Descriptive Note:
Final rept.
Pagination:
0029

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Monitor Series:
EOARD
 Subject Terms
Joint Capability Areas:
JCA_1_Force Support; JCA_1.2.6_Concepts; JCA_1.2_Force Preparation; JCA_3.2_Engagement; JCA_3_Force Application; JCA_1.4.2_Health Service Delivery; JCA_1.4_Force Support; JCA_3.2.1_Kinetic Means; JCA_5.3_Planning; JCA_5_Command and Control; JCA_8_Building Partnerships; JCA_6_Net Centric; JCA_8.2_Shape
Communities of Interest:
Air Platforms
Descriptor(s):
*AIR BREATHING ENGINES, *HYPERSONIC FLIGHT, AIR FLOW, GAS TURBINES, COMBUSTION CHAMBERS, RUSSIA, AEROTHERMODYNAMICS, FUEL BURN UP, SYNERGISM, AIR INTAKES, AXIAL FLOW COMPRESSORS
Field(s)/Group(s):
Jet and Gas Turbine Engines
Keyword(s):
FOREIGN REPORTS
Report Date:
1997 Aug 01
Creation Date:
1997 Oct 08