EXPERIMENTAL AND DESIGN STUDIES FOR TURBO-RAMJET COMBINATION ENGINE. VOLUME 4 - CALCULATED RESULTS

reportActive / Technical Report | Accession Number: AD0486378 | Open PDF

Abstract:

The calculation results are presented of the parametric investigation of the engine optimum operating point, that permits one to determine the performance characteristics of the power plant, and the laws of regulation of the internal variable cross-section areas flow mixer, exit nozzle throat and the characteristics of the internal flow speeds, temperatures, pressures, and flow rate ratios in the different stations.

Author(s):
Chaulin, P. ; Ravel, M. ; Gozlan, A.
Author Organization(s):
NORD AVIATION CHATILLON-SOUS-BAGNEUX (FRANCE)
Descriptive Note:
Final rept.
Supplementary Note:
See also Volume 5, AD484774.
Pagination:
0178

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):
5152/NIOBE-4/34/Z, 5153/NIOBE-4/35/Z
Contract/Grant Number(s):
AF 61(052)-750
Task Number(s):
301203
Project Number(s):
AF-3012
Monitor Series:
TR-66-34-VOL-4, AFAPL
 Subject Terms
Joint Capability Areas:
JCA_8_Building Partnerships; JCA_8.2_Shape; JCA_5_Command and Control; JCA_8.1_Communicate; JCA_5.2.2_Develop Knowledge and Situational Awareness; JCA_5.2_Understand
Communities of Interest:
Space
Descriptor(s):
*TURBORAMJET ENGINES, AFTERBURNING, AIRSPEED, ALTITUDE, DRAG, FLAME HOLDERS, FRANCE, FUEL CONSUMPTION, GAS FLOW, MIXTURES, NOZZLE THROATS, OPERATION, OPTIMIZATION, PERFORMANCE(ENGINEERING), PRESSURE, RAMJET ENGINES, SECONDARY FLOW, TEMPERATURE, THRUST, TURBOFAN ENGINES, VARIABLE AREA NOZZLES, VELOCITY
Field(s)/Group(s):
Jet and Gas Turbine Engines
Report Date:
1965 Jan 01