Pt 1: Series of power plants propelled partly by reaction effect, partly by turbine propellers, compared with each other and with Otto engine with respect to power concentration, fuel consumption, weight per unit power, etc. Pt 2: Influence of ram pressure, gas temperature, preheating of fuel, and pressure ratio on efficiency. English abstract from Deutsche Versuchsanstalt fuer Luftfahrt, Forschungsbericht n 1069 May 15, 1939.
Exhaust turbine and jet propulsion systems
Nat Advisory Committee Aeronautics -- Tech Memo
1951
48 pages
Diagrs, graphs, tables
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Exhaust turbine and jet propulsion systems
TIBKAT | 1951
|AIRCRAFT PROPULSION SYSTEM WITH TURBINE ENGINE AND EXHAUST CONDENSER
Europäisches Patentamt | 2024
|Aircraft propulsion system with turbine engine and exhaust condenser
Europäisches Patentamt | 2024
|Aircraft propulsion system with turbine engine and exhaust condenser
Europäisches Patentamt | 2024
|AIRCRAFT PROPULSION SYSTEM WITH TURBINE ENGINE AND EXHAUST CONDENSER
Europäisches Patentamt | 2024
|