Peak heating for reattachment of separated flow on a spiked blunt-body

Heat and Mass Transfer/Waerme- und Stoffuebertragung

Volumn 36, Issue 4, 2000, Pages 277-283

  Mehta, R C ^a  

^a INDIAN SPACE RESEARCH ORGANISATION   (India)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; DRAG; FINITE VOLUME METHOD; HEAT FLUX; NAVIER STOKES EQUATIONS; RUNGE KUTTA METHODS; SUPERSONIC AERODYNAMICS;

MACH NUMBER;

HEAT TRANSFER;

EID: 0034225203     PISSN: 09477411     EISSN: None     Source Type: Journal    
DOI: 10.1007/s002310000091     Document Type: Article

References (8)

1. Stalder JR; Nielsew HV (1954) Heat transfer from a hemisphere-cylinder equipped with flow-separated spikes. NACA TN 3287
2. Bogdonoff SM; Vas IE (1958) Preliminary investigations of spiked bodies at hypersonic speeds. Report Number 412, Dept. Aero. Engg., Princeton University
3. Chapman DR (1956) A theoretical analysis of heat transfer in region of separated flow. NACA TN 3792
4. Crawford DH (1959) Investigation of the flow over a spiked-nose hemisphere-cylinder at a Mach number of 6.8. NASA TN D-118
5. Yamauchi M; Fujii K; Tamura Y; Higashino F (1993) Numerical investigation of supersonic flows around a spiked blunt body. AIAA paper 93-0887
6. Peyret R; Vivind H (1993) Computational Methods for Fluid Flow, Springer-Verlag, 109-111
7. Jameson A; Schmidt W; Turkel E (1981) Numerical solution of Euler equations by finite volume methods using Runge-Kutta time stepping schemes. AIAA paper 81-1259
8. Shang JS (1981) Numerical simulation of wing-fuselage interference aerodynamic. AIAA paper 81-0084