Appearance of restricted shock separation in rocket nozzles

Journal of Propulsion and Power

Volumn 18, Issue 3, 2002, Pages 577-584

  Hagemann, Gerald ^a,c   Frey, Manuel ^b,d,e   Koschel, Wolfgang ^b,d,e  

^a AIRBUS DEFENCE AND SPACE   (Germany)

^b GERMAN AEROSPACE CENTER DLR   (Germany)

^c Daimler Chrysler Aerospace   (Germany)

^d VOLVO AERO CORPORATION   (Sweden)

^e Langer Grund   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

FLOW PATTERNS; LOADS (FORCES); NOZZLES; SHOCK WAVES;

SHOCK SEPARATION;

ROCKET ENGINES;

EID: 0036575609     PISSN: 07484658     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.5971     Document Type: Article

References (18)

1. Sea level side loads in high-area-ratio rocket engines
2. Flow separation and side-loads in rocket nozzles
3. Flow separation and side-loads in rocket nozzles
4. Restricted shock separation in rocket nozzles
5. A sub-scale test programme on investigation of flow separation and side-loads in rocket nozzles
6. A subscale investigation on side-loads in sea level rocket nozzles
7. Flow separation and side-load behaviour of the Vulcain engine
8. Numerical analysis of the performance of altitude compensating dual-bell nozzle flows
9. Subscale tests with an advanced 40 kN thrust chamber
10. Nozzle flowfield analysis with particular regard to 3D-plug-cluster configurations
11. Numerical study of an underexpanded jet
12. Electron beam fluorescence measurements of shock reflection hysteresis in an underexpanded supersonic jet
13. Gasdynamics: Theory and applications
14. Subscale nozzle testing at the P6.2 Test stand
15. Shock-induced boundary layer separation in overexpanded conical exhaust nozzles