Oblique wave disturbance analysis of supersonic flow past axisymmetric and 2D bodies at angles of attack

38th AIAA Fluid Dynamics Conference and Exhibit

Volumn , Issue , 2008, Pages

  Alba, Christopher E ^a,b   Johnson, Heath B ^a   Candler, Graham V ^a  

^a University of Minnesota   (United States)

^b USAF   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; INCOMPRESSIBLE FLOW; STABILITY; SUPERSONIC FLOW;

ACCURATE CALCULATIONS; ANGLES OF ATTACK; BOUNDARY LAYER STABILITY ANALYSIS; PARABOLIZED STABILITY EQUATIONS; SOFTWARE SUITE; STABILITY RESULTS; TOLLMIEN-SCHLICHTING INSTABILITY; TWO-DIMENSIONAL WAVES;

ANGLE OF ATTACK;

EID: 78049491480     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-4396     Document Type: Conference Paper

References (6)

1. Christopher R. Alba, Heath B. Johnson, Matthew D. Bartkowicz, and Graham V. Candler. Boundary Layer Stability Calculations of the HIFiRE Flight 1 Vehicle in the LaRC 20-Inch Mach 6 Air Tunnel. Paper 2008-505, AIAA, January 2008.
2. M.R. Malik and R.E. Spall. On the stability of compressible flow past axisymmetric bodies. Journal of Fluid Mechanics, 228:443-463, 1991.
3. Leslie M. Mack. Effect of cooling on boundary-layer stability at mach number 3. In D.E. Ashpis, T.B. Gatski, and R. Hirsh, editors, Instabilities and Turbulence in Engineering Flows, pages 175-188. Kluwer Academic Publishers, 1993.
4. H. B. Johnson and G. V. Candler. Hypersonic Boundary Layer Stability Analysis Using PSE-Chem. Paper 2005-5023, AIAA, June 2005.
5. M. J. Wright, G. V. Candler, and D. Bose. A Data-Parallel Line-Relaxation Method for the Navier-Stokes Equations. Paper 97-2046CP, AIAA, June 1997.
6. Leslie M. Mack. Boundary-layer linear stability theory. In Special Course on Stability and Transition of Laminar Flow, AGARD-R-709, chapter 3, pages 3-1:3-81. June 1984.