Evaluation of stability derivatives of an ogive in a Newtonian limit

Author:

Shabana Ayesha,Bayar Anitha Dayanand,Crasta Asha,Khan Sher Afghan,Baig Maughal Ahmed Ali,Reddy Voggu Kesava

Publisher

AIP Publishing

Reference24 articles.

1. Ghosh, K., 1977. A New Similitude for Aerofoils in Hypersonic Flow. Proceedings of the 6th Canadian Congress of Applied Mechanics, Vancouver, Canada, May 29-June 3, pp. 685–686.

2. Ghosh, K., 1984. Hypersonic large deflection similitude for oscillating delta wings. The Aeronautical Journal, pp. 357–361.

3. Khan, S. A., and Asha Crasta, 2010. Oscillating Supersonic delta wings with curved leading Edges. Advanced Studies in Contemporary Mathematics, 20(3), pp. 359–372.

4. Asha Crasta and S. A. Khan, 2013. Effect of Angle of Incidence on Stability derivatives of a Wing, IET Conference Publications

5. Asha Crasta, S. A. Khan, 2013 Determination of Surface Pressure of an axisymmetric ogive in Hypersonic Flow. Mathematical Sciences International Research Journal, Vol. 2, Issue 2, August 2013, pp.333–335, ISSN: 2278-8697.

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