Flow Separation in Rocket Nozzles – An Overview

The paper includes a literature overview on the history of separated rocket nozzle flow research as well as a data base on flow separation in convergent-divergent nozzles.

[1]  Gerald Hagemann,et al.  Flow Separation and Side-Load Behavior of the Vulcain Engine , 1999 .

[2]  Takeo Tomita,et al.  Transient Flow Simulation of a Compressed Truncated Perfect Nozzle , 2001 .

[3]  Joseph H. Ruf,et al.  Details of Side Load Test Data and Analysis for a Truncated Ideal Contour Nozzle and a Parabolic Contour Nozzle , 2010 .

[4]  Dimitri Papamoschou,et al.  Supersonic flow separation in planar nozzles , 2009 .

[5]  Gerald Hagemann,et al.  Scalability for Rocket Nozzle Flows Based on Subscale and Full-Scale Testing , 2003 .

[6]  H. Tsai,et al.  Numerical investigation of supersonic nozzle flow separation , 2007 .

[7]  R. A. Lawrence Symmetrical and unsymmetrical flow separation in supersonic nozzles , 1967 .

[8]  Andrew Beke,et al.  Thrust characteristics of a series of convergent-divergent exhaust nozzles at subsonic and supersonic flight speeds , 1954 .

[9]  G. Hagemann,et al.  Flow Separation and Side-Loads in Rocket Nozzles , 1999 .

[10]  H. L. G. Sunley,et al.  Jet Separation in Conical Nozzles , 1964, The Journal of the Royal Aeronautical Society.

[11]  S. Kalt,et al.  Conical rocket nozzle performance under flow- separated conditions , 1965 .

[12]  Tomas Damgaard,et al.  Side-Load Phenomena in Highly Overexpanded Rocket Nozzles , 2004 .

[13]  Carl E. Campbell,et al.  Performance of Several Method-of-Characteristics Exhaust Nozzles , 1960 .

[14]  E. Spiegler,et al.  Shock-Induced Boundary Layer Separation in Over-Expanded Conical Exhaust Nozzles , 1963 .

[15]  Kazumi Tsunoda,et al.  Improvement of the performance of a supersonic nozzle by riblets , 2000 .

[16]  R. J. Antl,et al.  EXPERIMENTAL STUDY OF EFFECTS OF GEOMETRIC VARIABLES ON PERFORMANCE OF CONICAL ROCKET-ENGINE EXHAUST NOZZLES , 1961 .

[17]  Luca Boccaletto,et al.  Solving the flow separation issue: a new nozzle concept. , 2008 .

[18]  Manuel Frey,et al.  Behandlung von Strömungsproblemen in Raketendüsen bei Überexpansion , 2001 .

[19]  J. M. Farley,et al.  Performance of Several Conical Convergent-Divergent Rocket-Type Exhaust Nozzles , 1960 .

[20]  Mikael Bigert,et al.  A Sub Scale Investigation on Side Loads in Sea Level Rocket Nozzles , 1999 .

[21]  Charles R. Foster,et al.  Experimental Study of Gas-Flow Separation in Overexpanded Exhaust Nozzles for Rocket Motors , 1949 .

[22]  Takeo Tomita,et al.  Visualization of the formation of separation bubbles on a bell-shaped nozzle surface in relation to serious side-load , 2001 .

[23]  Ralf Stark,et al.  Beitrag zum Verständnis der Strömungsablösung in Raketendüsen , 2010 .

[24]  Eugene S Love Pressure rise associated with shock-induced boundary-layer separation , 1955 .

[25]  Walter C. Swan The influence of nozzle design on the flight performance of rocket vehicles, with an analysis of the results of jet separation , 1948 .

[26]  Unsteady flow phenomena in nozzles , 1965 .

[27]  D. Blacodon,et al.  Flow separation experimental analysis in overexpanded subscale rocket-nozzles , 2001 .

[28]  Ralf Stark,et al.  Experimental study of boundary layer separation in truncated ideal contour nozzles , 2009 .

[29]  G. Hagemann,et al.  Status of Low Separation Prediction in Rocket Nozzles. , 1998 .

[30]  Gerald Hagemann,et al.  Shock pattern in the plume of rocket nozzles: needs for design consideration , 2008 .

[31]  S. Deck,et al.  Unsteady Side Loads in a Thrust-Optimized Contour Nozzle at Hysteresis Regime , 2004 .

[32]  Joseph H. Ruf,et al.  Nozzle Side Load Testing and Analysis at Marshall Space Flight Center , 2009 .

[33]  S. Verma Study of Flow Separation in Truncated Ideal Contour Nozzle , 2002 .

[34]  David Zerjeski,et al.  Semi-empirical Flow Separation Model For Overexpanded Rocket Nozzles , 2003 .

[35]  Craig A. Hunter,et al.  Experimental Investigation of Separated Nozzle Flows , 2004 .

[36]  L. H. Nave,et al.  Sea level side loads in high-area-ratio rocket engines , 1973 .

[37]  G. Rao Exhaust Nozzle Contour for Optimum Thrust , 1958 .

[38]  Abderrahmane Nebbache Aérodynamique d'un écoulement en tuyère idéale tronquée , 2007 .

[39]  K. Yonezawa,et al.  A Suppression Method of Restricted Shock Separation in Overexpanded Rocket Nozzle , 2006 .

[40]  Maurice Tucker,et al.  Effect of a Discontinuity on Turbulent Boundary-Layer-Thickness Parameters With Application to Shock-Induced Separation , 1955 .