Back
Other

Formulario gasdinamica

Study material for Aerothermodynamics, shared by the Studwiz community and reviewed by moderators.

AerothermodynamicsOther

Document information

What's included in this study material

Study material for Aerothermodynamics, shared by the Studwiz community and reviewed by moderators.

Import quality: text was extracted directly from the original document.

Extracted content from the document

Representative passages recognised in different parts of the material. The full extracted text remains available to search, while this compact preview makes the page easier to read.

Page 1

Termodinamica Relazioni di Maxwell: (∂T ∂v ) s = − (∂P ∂s ) v , (∂T ∂P ) s = (∂v ∂s ) P , (∂s ∂v ) T = (∂P ∂T ) v , (∂s ∂P ) T = − (∂v ∂T ) P Relazione di Reciprocit` a: (∂e ∂v ) T =T (∂P ∂T ) v −P, Derivata fondamentale della gasdinamica: Γ = c4 2v3 (∂2v ∂P 2 ) s Gas ideale politropico: s(e,v ) =s0 +R ln [ (e/e0) 1 γ−1 (v/v0) ] , e (s,v ) =e0 exp [(γ − 1)(s −s0)/R] (v/v0)γ−1 , ΓPIG = γ + 1 2 Gas di van der Waals: P (T,v ) = RT v −b − a v2, P c = a 27b2, T c = 8a 27bR, v c = 3b Acustica Intensit` a: Φe = c3 ρ0T ∫ T 0 ρ2 dt, ∆ = 10 log10 Φe Φe,ref , Φe,ref = 10−12W/m2 Correnti stazionarie isentropiche di gas ideale politropico T t T = [ 1 +γ − 1 2 M 2 ] , P t P = [ 1 +γ − 1 2 M 2 ] γ γ−1 , ρt ρ = [ 1 +γ − 1 2 M 2 ] 1 γ−1 , Onde d’urto Urto obliquo: ML,n =ML sinβ, M R,n =MRsin (β −θ), tanθ = 2 cotβ [ M 2 L sin2β − 1 M 2 L (γ + cos 2β) + 2 ] Gas Ideale Politropico: PR PL = γ+1 γ−1 − vR vL γ+1 γ−1 vR vL − 1, ρR ρL = (γ + 1)M 2 L,n (γ − 1)M 2 L,n + 2, M 2 R,n = M 2 L,n + 2 γ−1 2γ γ−1M 2 L,n − 1 (P t R P t L )γ−1 = [ (γ+1)M 2 L (γ−1)M 2 L+2 ]γ 1 + 2γ γ+1(M 2 L − 1), wR −wL cL = − 2 γ + 1 [ ML,n − 1 ML,n ] PR −PL PL = 2γ γ + 1 ( M 2 L,n − 1 ) , vR −vL vL = − 2 γ + 1 [ 1 − 1 M 2 L,n ] Correnti stazionarie non viscose quasi-monodimensionale Corrente isentropica : A A0 = M0 M [ 1 + γ−1 2 M 2 1 + γ−1 2 M 2 0 ] γ+1 2(γ−1) Urto nel divergente: M 2 e = −1 − √ 1 + 2β2(γ − 1) γ − 1 , β = P t Pa Ag Ae [ 2 γ + 1 ] γ+1 2(γ−1) Correnti stazionarie non viscose bidimensionali Correnti transoniche: ( K −φξ)φξξ +φηη = 0, K = (1 −M 2 ∞)M − 4 3 ∞ (2Γ∞s)− 2 3 Metodo di Sauer: f0(x) = 1 2αx2, α = √ 1/(2Γ∞rtyt), ϵ =xt + 1 3Γ∞αy2 t Funzione di Prandtl-Meyer: ν(M) = √γ + 1 γ − 1 tan−1 [√γ − 1 γ + 1(M 2 − 1) ] − tan−1 [√ M 2 − 1 ] , v lim = Π 2 [√γ + 1 γ − 1 − 1 ] Correnti di F anno 4 ¯fL MAX D = 1…

Preview

First page of the document.

First page: Formulario gasdinamica