THE INVESTIGATION OF A RESONANT WAVE ENGINE

reportActive / Technical Report | Accession Number: AD0129618 | Open PDF

Abstract:

This report summarizes theoretical and experimental Investigations of a new font of intermittent heat engine employing pressure waves for compression prior to heat addition, which were carried oat at Cornell Aeronautical Laboratory between november 1951 and November 1955.

Author(s):
Russo, A. L. ; Hertzberg, A. ; Logan, J. G.
Author Organization(s):
CORNELL AERONAUTICAL LAB INC BUFFALO NY
Supplementary Note:
DOI: 10.21236/AD0129618
Pagination:
0069

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):
DD-799-A-3
Contract/Grant Number(s):
NONR-665(00)
Monitor Series:
ONR
 Subject Terms
Joint Capability Areas:
JCA_4.7.2_Installation Services; JCA_4.7_Base and Installations Support; JCA_5.3_Planning; JCA_5_Command and Control; JCA_3.2_Engagement; JCA_3_Force Application; JCA_1.2.7_Experimentation; JCA_3.2.1_Kinetic Means
Modernization Areas:
Hypersonics
Communities of Interest:
Weapons Technologies
Descriptor(s):
*PULSEJET ENGINES
Field(s)/Group(s):
Jet and Gas Turbine Engines
Report Date:
1956 Aug 01