Asha Crastaa
Asha Crastaa
Mangalore Institute of Technology and Engineering
Verified email at mite.ac.in
Title
Cited by
Cited by
Year
osCIILATING SUPERsoNIC DELA WINGs. w CURVED LEADING EDGES
SA Khan, A Crasta
322010
Oscillating Supersonic delta wing with straight Leading Edges
A Crasta, SA Khan
International Journal of Computational Engineering Research 2 (5), 1226-1233, 2012
312012
High Incidence Supersonic similitude for Planar wedge
A Crasta, SA Khan
International Journal of Engineering research and Applications 2 (5), 468-471, 2012
282012
Stability Derivatives in the Newtonian Limit
A Crasta, SA Khan
International Journal of Advanced Research in Engineering and Technology 4 …, 2013
252013
Estimation of Stability derivatives of a Delta wing in Hypersonic flow
A Crasta, MA Baig, SA Khan
International Journal of Emerging trends in Engineering and Developments 6 …, 2012
252012
Hypersonic similitude for planar wedges
A Crasta, SA Khan
International Journal of Advanced Research in Engineering and Technology 5 …, 2014
242014
Effect of Angle of Incidence on Stability derivatives of a wing
A Crasta, SA Khan
IET Digital Library, 2013
242013
EFFECT OF ANGLE OF INCIDENCEON ROLL DAMPING DERIVATIVE OF A DELTA WING
A Crasta, SA Khan
212014
Effect of Mach number on Stiffness and Damping Derivatives for Oscillating Hypersonic Non-Planar Wedge
A Crasta, SA Khan
IOSR Journal of Mechanical and Civil Engineering 11 (2), 04-11, 2014
202014
Supersonic Similitude for Oscillating Non-Planar wedge
A Crasta, SA Khan
IOSR Journal of Mathematics 10 (2), 15-24, 2014
202014
Effect of Angle of Incidence on Stiffness and Damping derivatives for Oscillating Hypersonic Non-planar Wedge
A Crasta, SA Khan
International Journal for Research in Applied Science and Engineering …, 2014
192014
Estimation of Stability Derivatives for a Planar Wedge in the Newtonian Limit
A Crasta, SA Khan
IOSR Journal of Mathematics 10 (2), 01-06, 2014
192014
„Stability derivatives of a Delta Wing with Straight leading edge in the Newtonian Limit‟
A Crasta, SA Khan
International Journal of Engineering research and Applications 4 (3), 32-38, 2014
182014
„Effect of sweep angle on Roll damping derivative of a Delta Wing‟
A Crasta, SA Khan
International Journal of Emerging trends in Engineering and Developments 5 …, 2014
152014
Estimation of Stability derivatives of an Oscillating Hypersonic delta wings with curved leading edges
A Crasta, SA Khan
International Journal of Mechanical Engineering & Technology 3 (3), 483-492, 2012
152012
Effect of Angle of attack on Stiffness derivative of an oscillating supersonic delta wing with curved leading edges
A Crasta, SA Khan
IOSR-JMCE issue1, Volume12, December, pp12-25, 2015
122015
Effect of Angle of attack on Stability derivatives of a Delta wing with Straight leading edge in Supersonic Flow‟
A Crasta, SA Khan
International Journal of Mathematics 10 (5), 01-08, 2014
122014
Effect of Angle of attack on Stability Derivatives of a Delta wing in Hypersonic Flow with Straight leading edge‟
A Crasta, SA Khan
International Journal of Mechanical and civil engineering 11 (5), 21-29, 2014
122014
Estimation of Surface Pressure Distribution On a Delta Wing with Curved Leading Edges in Hypersonic/Supersonic Flow
A Crasta, S Pavitra, SA Khan
International Journal of Energy, Environment and Economics 24 (1), 67-73, 2016
102016
Estimation of Stability Derivatives in Newtonian Limit for Oscillating Cone
A Shabana, RS Monis, A Crasta, SA Khan
IOP Conference Series: Materials Science and Engineering 370 (1), 012061, 2018
82018
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