Accession Number:

AD0056235

Title:

Theoretical studies of the Performance of Heat Engines Using Pressure Waves

Personal Author(s):

Corporate Author:

CORNELL AERONAUTICAL LAB INC BUFFALO NY

Report Date:

1954-12-01

Abstract:

Theoretical performance investigations have been undertaken for a number of wave-engine configurations using the techniques of the method of characteristics. The use of these nonsteady flow techniques permits a determination of intermittent engine performance parameters such as thrust per unit area, specific fuel consumption, compression efficiency and cycle time which are much more realistic than those obtained by the use of the conventional quasi-steady or steady-flow methods.

Supplementary Note:

DOI: 10.21236/AD0056235

Pages:

0206

Communities Of Interest:

Contract Number:

NONR-665(00)

File Size:

9.80MB