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Shock Reduction Through Active Flow Control: Aerodynamic and Flight Stability Considerations / Shagufta Rashid

TextIslamabad; SINES NUST; 2022Description: 180,p; ill; 30,cmSubject(s): PhD- Computation Science & EngineeringDDC classification: 200 Online resources: Click here to access online

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Item type	Current location	Home library	Shelving location	Call number	Status	Date due	Barcode	Item holds
Soft Copy	Central Library (CL)	Central Library (CL)	Thesis	200 (Browse shelf)	Available		CLPT-393

Total holds: 0

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Previous	200 Molecular Modeling Strategies to Design Novel Inhibitors of GAT1/	200 Structural and regulatory analysts of ANGPTLS using computational approaches and the formal verification of its biological regulatory network in insulin reslstance/	200 Dynamics, Numerical Optimization and Control of Dynamic Soaring Maneuvers for a Morphing Capable Unmanned Aerial Vehicle/	200 Shock Reduction Through Active Flow Control: Aerodynamic and Flight Stability Considerations /	200 Dynamical Modelling and Analysis of mTOR associated Biological Networks in Survival Mechanisms/	200 Computational Modelling and Analysis of Neuronal Pathways in Alzheimer’s/	200 Combined Ligand and Structure Based Studies on Modulators of Akt Kinases/	Next

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