Investigation of the Effect of Booster Attachment Scheme on the Rolling Moment Characteristics of an Asymmetric Vehicle Using CFD

Author:

Sinha P. K.,Ralh Munish Kumar,Ali Naveed,Krishnamohan Rao R.,Balu G.

Publisher

Springer Singapore

Reference6 articles.

1. Ralh MK, Sinha PK, Theerthamalai P (2017) Aerodynamic characteristics of an Aerospace vehicle with side mounted air-intake in closed condition at subsonic and supersonic flow. In: Proceedings NCWT-05, MIT, Chennai, Mar 2017

2. Nath B, Sreenivasan N, Sampath Rao B Force measurement on a 1:3.56 scale model of SFDR configuration. Doc. No. PD-NTF/2016/1011

3. Auman LM, Kreegar RE Aerodynamic characteristics of a canard controlled missile with a free spinning tail. AIAA-1998–0410

4. Sreenivasan N, Nath B, Joshi K, Sampath Rao B Force measurement on 1:10.2 scale model of SFDR with ground booster configuration. Doc. No. PD-NTF/2017/1014

5. User’s Manual for NUMECA-FINE/Hexa V2.10–4”, Numeca International, Brussels, Belgium

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