Generalization of turbojet-engine performance in terms of pumping characteristics / Newell D. Sanders and Michael Behun.
Characteristics of a basic turbojet engine consisting of compressor, combustor, and turbine can be presented in terms of pumping characteristics; that is, corrected air flow, ratio of engine-outlet to -inlet total pressure, ratio of engine-outlet to -inlet total temperature, Reynolds number index, c...
Saved in:
| Online Access: |
Search for the full-text version of this title in HathiTrust |
|---|---|
| Main Author: | |
| Corporate Author: | |
| Other Authors: | |
| Other title: | Technical report archive and image library. |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1949.
|
| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
1927. |
| Subjects: |
Internet
Search for the full-text version of this title in HathiTrustPASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/1927
|
|---|---|
| Y 3.N 21/5:6/1927 | Available Place a Hold |