Plif imaging of hypersonic reactive flow around blunt bodies

Symposium (International) on Combustion

Volumn 26, Issue 2, 1996, Pages 2909-2915

  Kamel, M R ^a   Morris, C I ^a   Stouklov, I G ^a   Hanson, R K ^a  

^a STANFORD UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; DETONATION; ETHYLENE; FLUORESCENCE; HYDROGEN; HYPERSONIC FLOW; IMAGING TECHNIQUES; METHANE; SHOCK WAVES; VELOCITY;

BLUNT BODIES; PLANAR LASER INDUCED FLUORESCENCE; SCHLIEREN IMAGING; WEDGE;

FLOW VISUALIZATION;

EID: 0030374204     PISSN: 00820784     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0082-0784(96)80132-9     Document Type: Article

References (18)

1. New Expansion Tube Facility for the Investigation of Hypersonic Reactive Flow
2. Development of an Expansion Tube for Investigation of Combustion in Supersonic Projectile Flowfields
3. Ram accelerator - A new chemical method for accelerating projectilesto ultrahigh velocities
4. H2-air and CH4-air detonations and combustions behindoblique shock waves
5. Examination of the Improved Model for the Unsteady Combustion around Hypersonic Projectiles
6. A Preliminary Theoretical Study of the Expansion Tube, A New Device for Producing High-Enthalpy Short-Duration Hypersonic Gas Flows
7. PLIF Imaging of Transient Shock Phenomena in Hypersonic Flows
8. On the Initiation of Detonation by a Hypervelocity Projectile