WASET
	@article{(Open Science Index):https://publications.waset.org/pdf/14786,
	  title     = {An Approximate Engineering Method for Aerodynamic Heating Solution around Blunt Body Nose},
	  author    = {Sahar Noori and  Seyed Amir Hossein and  Mohammad Ebrahimi},
	  country	= {},
	  institution	= {},
	  abstract     = {This paper is devoted to predict laminar and turbulent
heating rates around blunt re-entry spacecraft at hypersonic
conditions. Heating calculation of a hypersonic body is normally
performed during the critical part of its flight trajectory. The
procedure is of an inverse method, where a shock wave is assumed,
and the body shape that supports this shock, as well as the flowfield
between the shock and body, are calculated. For simplicity the
normal momentum equation is replaced with a second order pressure
relation; this simplification significantly reduces computation time.
The geometries specified in this research, are parabola and ellipsoids
which may have conical after bodies. An excellent agreement is
observed between the results obtained in this paper and those
calculated by others- research. Since this method is much faster than
Navier-Stokes solutions, it can be used in preliminary design,
parametric study of hypersonic vehicles.},
	    journal   = {International Journal of Aerospace and Mechanical Engineering},
	  volume    = {6},
	  number    = {10},
	  year      = {2012},
	  pages     = {2221 - 2225},
	  ee        = {https://publications.waset.org/pdf/14786},
	  url   	= {https://publications.waset.org/vol/70},
	  bibsource = {https://publications.waset.org/},
	  issn  	= {eISSN: 1307-6892},
	  publisher = {World Academy of Science, Engineering and Technology},
	  index 	= {Open Science Index 70, 2012},
	}