Influence of spike shape at supersonic flow past blunt-nosed bodies: Experimental study

AIAA Journal

Volumn 40, Issue 5, 2002, Pages 1018-1020

  Milićev, Snežana S ^a   Pavlović, Miloš D ^a  

^a UNIVERSITY OF BELGRADE   (Serbia)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BOUNDARY LAYER FLOW; DRAG; FLOW VISUALIZATION; MATHEMATICAL MODELS; SHOCK WAVES;

DRAG COEFFICIENT;

SUPERSONIC FLOW;

EID: 0036572665     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1745     Document Type: Article

References (7)

1. Transonic flow modes of an axisymmetric blunt body
2. Flow separation on thin protruding probes placed in front of blunt bodies at supersonic/hypersonic speeds
3. Drag and lift control
4. Modes of shock-wave oscillations on spike-tipped bodies
5. Preliminary investigations of spiked bodies at hypersonic speeds
6. Equations, tables, and charts for compressible flow