Evaluation of aerospike for drag reduction on a blunt nose using experimental and numerical modeling

Author:

Esfeh Mohamad Kazemi,Tajalli Seyed Mohamad,Liu Pengfei

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference41 articles.

1. Flow separation ahead of a blunt axially symmetric body at mach numbers 1.76 to 2.10;Moeckel,1951

2. Experiments on separation of boundary layers on probes in front of blunt-nosed bodies in a supersonic air stream;Mair;Philos. Mag.,1952

3. Fluid–Thermal interaction investigation of spiked blunt bodies at hypersonic flight condition;Guo;J. Spacecr. Rocket.,2016

4. Preliminary investigations of spiked bodies at hypersonic speeds;Bogdonoff;J. Aerosp. Sci.,1959

5. Aerodynamic spike flowfields computed to select optimum configuration at mach 2.5 with experimental validation;Shoemaker,1990

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