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. & 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., & 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
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, 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.
