نمایش نتایج جستجو برای
کلمات کلیدی: Mach Number
موارد یافت شده: 9
1 - Performance Enhancement of a Supersonic Air Intake by Applying a Heat Source (چکیده)2 - Experimental investigation into the effects of Mach number and boundary-layer bleed on flow stability of a supersonic air intake (چکیده)
3 - Compressibility effects on the flow past a rotating cylinder (چکیده)
4 - Investigation of Corner Rounding Effects on the Performance of a Supersonic Air Intake (چکیده)
5 - Axisymmetric Stagnation Flow and Heat Transfer of a Compressible Fluid Impinging on a Cylinder Moving Axially (چکیده)
6 - Effects of Boundary-Layer Bleed Parameters on Supersonic Intake Performance (چکیده)
7 - STALL SIMULATION OF FLOW AROUND AN AIRFOIL USING LES MODEL AND COMPARISON OF RANS MODELS AT LOW ANGLES OF ATTACK (چکیده)
8 - STALL SIMULATION OF FLOW AROUND AN AIRFOIL USING LES MODEL AND COMPARISON OF RANS MODELS AT LOW ANGLES OF ATTACK (چکیده)
9 - Comparison between Scalar, CUSP and AUSM family Schemes in Low and High Mach numbers (چکیده)
