In the following paper, the effects of a choked jet exhausted from the base of a non-lifting body on its total and base drags at sub-sonic and transonic regimes has been numerically investigated. Having surveyed the results of some turbulence models and after comparing with experimental results, an appropriate turbulence model i.e. SST K-?, has been chosen and this model has been used in the subsequent analysis. The analysis have been conducted in the free stream Mach number range of 0.4
Saniei Nejad,M. and Jamshidi,R. (2010). Critical Drag Investigation for an Axisymmetric Projectile with Choked Base Bleed at High-Subsonic and Transonic Regime Using SST K-? Model. Journal of Aerospace Science and Technology, 7(1), 31-40.
MLA
Saniei Nejad,M. , and Jamshidi,R. . "Critical Drag Investigation for an Axisymmetric Projectile with Choked Base Bleed at High-Subsonic and Transonic Regime Using SST K-? Model", Journal of Aerospace Science and Technology, 7, 1, 2010, 31-40.
HARVARD
Saniei Nejad M., Jamshidi R. (2010). 'Critical Drag Investigation for an Axisymmetric Projectile with Choked Base Bleed at High-Subsonic and Transonic Regime Using SST K-? Model', Journal of Aerospace Science and Technology, 7(1), pp. 31-40.
CHICAGO
M. Saniei Nejad and R. Jamshidi, "Critical Drag Investigation for an Axisymmetric Projectile with Choked Base Bleed at High-Subsonic and Transonic Regime Using SST K-? Model," Journal of Aerospace Science and Technology, 7 1 (2010): 31-40,
VANCOUVER
Saniei Nejad M., Jamshidi R. Critical Drag Investigation for an Axisymmetric Projectile with Choked Base Bleed at High-Subsonic and Transonic Regime Using SST K-? Model. Journal of Aerospace Science and Technology, 2010; 7(1): 31-40.
