Experimental and analytical design verification of the dual-bell concept

Journal of Propulsion and Power

Volumn 18, Issue 1, 2002, Pages 116-122

  Hagemann, Gerald ^a   Terhardt, Michael ^a   Haeseler, Dietrich ^a   Frey, Manuel ^a  

^a AIRBUS DEFENCE AND SPACE   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMBUSTION CHAMBERS; HEAT FLUX; HEAT TRANSFER; MACHINE DESIGN;

DUAL-BELL NOZZLES;

NOZZLES;

EID: 0036155449     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5905     Document Type: Article

References (16)

1. Numerical analysis of the performance of altitude compensating dual-bell nozzle flows
2. Propulsion research for rocket SSTOs at NAL/KRC
3. FESTIP technology developments in liquid rocket propulsion for reusable launch vehicles
4. Critical assessment of dual-bell nozzles
5. Development of advanced technologies for future cryogenic thrust chamber applications
6. Numerical prediction of flow separation for advanced nozzle concept applications
7. Dual-bell nozzles for rocket engines of launch vehicle upper stages and orbital transfer vehicles
8. Restricted shock separation in rocket nozzles
9. Flow separation and side-loads in rocket nozzles
10. Subscale nozzle testing at the P6.2 test stand
11. A subscale investigation on side-loads in sea-level rocket nozzles
12. Flow separation and side-load behavior of the vulcain engine
13. Nozzle flowfield analysis with particular regard to three-dimensional plug-cluster configurations