Isentropic Relations,Normal Shock,Oblique Shock,Vortex Lattice Method,Pitot Tube
1. Calculadora aerodinâmica básica- Cálculo da pressão dinâmica, número de Reynolds, coeficiente de força e momento para o fluxo incompressível e compressível.
2. Isentropic Relations - If any one of the variables, M, Po/P, To/T, Rho/Rh or A/A* is known the remaining variable values can be computed.
3. CHOQUE NORMAL- Selecione qualquer variável conhecida da lista, M1, P2/P1, T2/T1, M2, Rho2/Rho1, PO2/PO1 e PO2/P1 e Usuário podem calcular os valores variáveis restantes. Indices 1 and 2 are for before shock and after shock respectively.
4. Oblique Shock - Theta-Beta-Mech number relation. If values of any two variable known then user can calculate value of remaining one.
5. Vortex Lattice Method - Vortex Lattice Method is a method used to calculate lift coefficient of Finite Wing at low speed. It gives fairly good CL estimation for Swept wing compared to Vortex Panel Method. This tool is helpful for primary aerodynamic design iterations. The method presented here uses 'n' spanwise divisions and one chordwise division of wing. The final output is slope of CL vs Alpha curve and it is CL per degree angle of attack.
6. Prandtl-Meyer expansion wave relations - Compute v1 from M1 (Mach Number before expansion wave). v is Prandtl-Meyer function. Add deflection angle theta to v1 to get v2. From v2 compute M2 (Mach Number after expansion wave).
7. Pitot Tube - Divided in two categories. One for Incompressible Flow and Other for Compressible Flow. Em caso de fluxo incompressível, o usuário pode inserir a altura da coluna do tubo pitot em metros de água, mercúrio ou qualquer fluido conhecido para calcular a velocidade do fluxo livre. The compressible flow case takes inputs for Total Pressure and Static Pressure measured by Pitot Tube and calculates Free Stream Mach Number. User need not to worry about Subsonic or Supersonic flows. These are identified and solved accordingly.
8. Y Plus or Y+ - It calculates first cell height of grid near wall to resolve boundary layer.
9. Check points for Inputs to avoid wrong inputs and flash suggestions if any.
If you like this, please consider buying ad-free version which can take any value of Specific Heat Ratio (Gamma) and not fixed to 1.4.
If found any Bug or wrong output, please mail me regarding issue
Antes de fornecer classificação negativa para anúncios pop-up, considere que tentei manter os anúncios quando o usuário terminar usando qualquer um da utilidade deste aplicativo e não no lançamento do utilitário, o que é mais censurável.
...Desde já, obrigado
Also released an app for solving compressible nozzle flow problem. Please go through it.
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