On the Equations of Nonstationary Transonic Gas Flows

The method of point transformation of the functions and variables for construction of particular solutions of the Equations of Nonstationary Transonic Gas Flows is used.

Authors: Valerii Dryuma

On the Equations of Nonstationary T ransonic Gas Flo ws V aleri i Dryuma ∗ Institute of Mathem atics and Informatics, AS RM, 5 A c ademiei Str e et, 20 28 Kishinev, Moldova , e-mail: v alery@dryuma.c o m; c a inar@mail.md Abstract The examples of solutio ns of the Equations of No nstationary T ransonic Gas Flo ws are considered. Their pr op erties are discussed. 1 In tro duction Tw o-dimensional equation of Nonstationary T ransonic Gas F lo w ha s the form 2 ∂ 2 ∂ x∂ z f ( x, y , z ) + ∂ ∂ x f ( x, y , z ) ! ∂ 2 ∂ x 2 f ( x, y , z ) − ∂ 2 ∂ y 2 f ( x, y , z ) = 0 , (1) where v a riable z is considered as the time-v ariable . Three-dimensional generalization of this equation is defined b y the equation 2 ∂ 2 ∂ x∂ z f ( x, y , z , s ) + ∂ ∂ x f ( x, y , z , s ) ! ∂ 2 ∂ x 2 f ( x, y , z , s ) − ∂ 2 ∂ y 2 f ( x, y , z , s ) − − ∂ 2 ∂ s 2 f ( x, y , z , s ) = 0 . (2) where v a riable z here is considered as the time-v ariable. The solutions of these equations and a corresp onding bibliograph y ha v e b een considered re- cen tly in [1] In this article we apply the metho d o f solution of the p.d.e.’s describ ed first in [2] and dev elop ed then in [3], [4]. This metho d allo w us to c onstruct particular solutions of the partial nonlinear differen tia l equation F ( x, y , z , f x , f y , f z , f xx , f xy , f xz , f y y , f y z , f xxx , f xy y , f xxy , .. ) = 0 . (3) ∗ W ork supp orted in part by Grant RFFI, Rus s ia-Moldov a 1 with the help of transformation of the function and v ariables. Essence of metho d consists in a follow ing presen tation of t he functions and v aria bles f ( x, y , z , s ) → u ( x, t, z , s ) , y → v ( x, t, z , s ) , f x → u x − u t v t v x , f s → u s − u t v t v s , f z → u z − u t v t v z , f y → u t v t , f y y → ( u t v t ) t v t , f xy → ( u x − u t v t v x ) t v t , ... (4) where v a riable t is considered as parameter. Remark that conditions of the type f xy = f y x , f xz = f z x , f xs = f sx ... are fulfilled at the suc h type of presen tat io n. In result instead of equation (3) one g et the relation b et we en the new v a riables u ( x, t, z ) and v ( x, t, z ) a nd their partial deriv atives Ψ( u, v , u x , u z , u t , u s , v x , v z , v t , v s ... ) = 0 . (5) This relation coincides with init ia l p.d.e at t he condition v ( x, t, z , s ) = t a nd ta kes more general form after presen tation of the functions u, v in fo r m u ( x, t, z , , s ) = F ( ω , ω t ... ) and v ( x, t, z , s ) = Φ( ω , ω t ... ) with some function ω ( x, t, z , s ) . Example. The equation of Riemann w a ve ∂ ∂ x f ( x, y ) + f ( x, y ) ∂ ∂ y f ( x, y ) = 0 after ( u, v )-transformatio n tak es the form ∂ ∂ x u ( x, t ) ! ∂ ∂ t v ( x, t ) − ∂ ∂ t u ( x, t ) ! ∂ ∂ x v ( x, t ) + u ( x, t ) ∂ ∂ t u ( x, t ) = 0 . The substitution here o f the expressions v ( x, t ) = t ∂ ∂ t ω ( x, t ) − ω ( x, t ) , u ( x, t ) = ∂ ∂ t ω ( x, t ) giv e us the linear equation ∂ ∂ x ω ( x, t ) + ∂ ∂ t ω ( x, t ) = 0 with general solution ω ( x, t ) = F1 ( t − x ) , where F1 ( t − x ) is arbitrary function. Choice of the function F1 ( t − x ) and elimination of the parameter t from the relations y − t D( F1 )( t − x ) + F1 ( t − x ) = 0 , f ( x, y ) − D( F1 )( t − x ) = 0 lead to the function f ( x, y ) satisfying the R iemann w av e equation. 2 2 Tw o-dimensi onal case The equation (1) after applying ( u, v )- transfor ma t ion with conditions u ( x, t, z ) = t ∂ ∂ t ω ( x, t, z ) − ω ( x, t, z ) and v ( x, t, z ) = ∂ ∂ t ω ( x, t, z ) tak es the form ∂ 2 ∂ t 2 ω ( x, t, z ) ! ∂ ∂ x ω ( x, t, z ) ! ∂ 2 ∂ x 2 ω ( x, t, z ) − 1 − 2 ∂ 2 ∂ t 2 ω ( x, t, z ) ! ∂ 2 ∂ x∂ z ω ( x, t, z )+ +2 ∂ 2 ∂ t∂ x ω ( x, t, z ) ! ∂ 2 ∂ t∂ z ω ( x, t, z ) − ∂ 2 ∂ t∂ x ω ( x, t, z ) ! 2 ∂ ∂ x ω ( x, t, z ) = 0 . (6) Its solution of the form ω ( x, t, z ) = A ( t, z ) − xB ( t ) lead to the equation on the function A ( t, z ) − 1 − 2 d dt B ( t ) ! ∂ 2 ∂ t∂ z A ( t, z ) + d dt B ( t ) ! 2 B ( t ) = 0 with solution A ( t, z ) = F2 ( t ) + F1 ( z ) +   − 1 / 2 Z d dt B ( t ) ! − 1 dt + 1 / 4 ( B ( t )) 2   z where F2 ( t ) , B ( t ) , F1 ( z ) are a rbitrary functions. In result w e find that the function ω ( x, t, z ) = F2 ( t ) + F1 ( z ) +   − 1 / 2 Z d dt B ( t ) ! − 1 dt + 1 / 4 ( B ( t )) 2   z − xB ( t ) is the solution of the equation (6). After the c hoice of the functions F2 ( t ) , B ( t ) and elimination of the par a meter t fro m the relations f − t ∂ ∂ t ω ( x, t, z ) − ω ( x, t, z ) ! = 0 y − ∂ ∂ t ω ( x, t, z ) = 0 one gets the solution of the equation (1). Let us consider some examples. In the case F2 ( t ) = 0 , B ( t ) = t − 1 , w e find the relations 4 f ( x, y , z ) t 2 − 4 / 3 z t 5 − 8 xt + 3 z + 4 F1 ( z ) t 2 = 0 , 3 and 2 y t 3 − z t 5 − 2 xt + z = 0 . Elimination of the pa r a meter t from these relat io ns in the case F1 ( z ) = 0 lead to the solutio n f ( x, y , z ) of the equation (1) satisfying the a lg ebraic equation 248832 ( f ( x, y , z )) 5 z 2 − 248 832 x 2 ( f ( x, y , z )) 4 z +  − 1451520 z 2 xy − 221184 y 3 z  ( f ( x, y , z )) 3 + +  − 216000 z 4 x + 475200 z 3 y 2 + 1327 104 y z x 3 + 2211 84 y 3 x 2  ( f ( x, y , z )) 2 + +  90000 y z 5 + 9953 28 y 4 z x + 6 14400 z 3 x 3 + 1290 240 y 2 z 2 x 2  f ( x, y , z ) − − 518400 y 3 z 3 x − 3 93216 x 5 z 2 − 117 9648 x 4 y 2 z + 31 25 z 7 − 373 248 y 5 z 2 − − 192000 z 4 x 2 y − 88473 6 y 4 x 3 = 0 . 3 Three-dimen sional generalizati on In a thr ee dimensional case the equation of Nonstationary T ransonic Ga s F lo w tak es the form 2 ∂ 2 ∂ x∂ z f ( x, y , z , s ) + ∂ ∂ x f ( x, y , z , s ) ! ∂ 2 ∂ x 2 f ( x, y , z , s ) − − ∂ 2 ∂ y 2 f ( x, y , z , s ) − ∂ 2 ∂ s 2 f ( x, y , z , s ) = 0 . (7) Recall that the v ariable z in this equation play the role o f a time-v a r ia ble. After application of u , v - transformation of the form u ( x, t, z , s ) = t ∂ ∂ t ω ( x, t, z , s ) − ω ( x, t, z , s ) , v ( x, t, z , s ) = ∂ ∂ t ω ( x, t, z , s ) w e find from ( 7) the equation ∂ 2 ∂ t 2 ω ( x, t, z , s ) ! ∂ 2 ∂ s 2 ω ( x, t, z , s ) − 2 ∂ 2 ∂ t 2 ω ( x, t, z , s ) ! ∂ 2 ∂ x∂ z ω ( x, t, z , s )+ + ∂ 2 ∂ t 2 ω ( x, t, z , s ) ! ∂ ∂ x ω ( x, t, z , s ) ! ∂ 2 ∂ x 2 ω ( x, t, z , s ) − − ∂ 2 ∂ t∂ x ω ( x, t, z , s ) ! 2 ∂ ∂ x ω ( x, t, z , s ) + 2 ∂ 2 ∂ t∂ x ω ( x, t, z , s ) ! ∂ 2 ∂ t∂ z ω ( x, t, z , s ) − − 1 − ∂ 2 ∂ s∂ t ω ( x, t, z , s ) ! 2 = 0 . (8) F rom here in the case ω ( x, t, z , s ) = A ( t, s ) + k ( x + z ) t one gets the Monge-Amp ere equation on the function A ( t, s ) 1 − ∂ 2 ∂ t 2 A ( t, s ) ! ∂ 2 ∂ s 2 A ( t, s ) + ∂ 2 ∂ s∂ t A ( t, s ) ! 2 = 0 . (9) 4 It is p ossible to sho w that the equation (9) can b e in tegrated with the help of corresp onding ( u, v )-transformation. Its solutions are dep enden t from solutions of the linear Laplace equation. In fact, the equation ∂ 2 ∂ x 2 f ( x, y ) ! ∂ 2 ∂ y 2 f ( x, y ) − ∂ 2 ∂ x∂ y f ( x, y ) ! 2 − 1 = 0 after ( u, v )-transformatio n with u ( x, t ) = tω t − ω , v ( x, t ) = ω t tak es the form o f linear Laplace equation ∂ 2 ∂ x 2 ω ( x, t ) + ∂ 2 ∂ t 2 ω ( x, t ) = 0 and its particular solutions after elimination of para meter t giv e us the solutions of the Monge- Amp ere equation (9). The substitution of a nother form ω ( x, t, z , s ) = A ( t, z ) + ( s + x ) t in to the equation (8) lead to the equation o n the function A ( t, z ) − 2 − t + 2 ∂ 2 ∂ t∂ z A ( t, z ) = 0 ha ving the general solution A ( t, z ) = F2 ( t ) + F1 ( z ) + tz + 1 / 4 t 2 z where F2 ( t ) , F1 ( z ) are arbitrary functions. The choice of the functions F2 ( t ) , F1 ( z ) allo w us to construct solutions of initia l equation. F or example in t he case F2 ( t ) = t − 1 , F1 ( z ) = 0 elimination of the parameter t fro m the r elat io ns 4 f ( x, y , z , s ) t − t 3 z + 8 = 0 , 2 y t 2 − 2 t 2 z − t 3 z − 2 t 2 s − 2 t 2 x + 2 = 0 giv e us the solution of the equation (7) satisfying the alg ebraic equation 16 ( f ( x, y , z , s )) 3 z + +  32 z y − 32 z x − 32 z s − 32 sx + 32 sy − 16 y 2 − 16 z 2 − 16 s 2 − 16 x 2 + 32 y x  ( f ( x, y , z , s )) 2 + +  72 z y − 72 z x − 72 z 2 − 72 z s  f ( x, y , z , s ) + 192 z s 2 + 64 s 3 − 64 y 3 − − 384 z y x + 384 z sx − 384 z y s + 27 z 2 + 192 sx 2 + 64 x 3 + 64 z 3 + 192 z 2 s + 192 z 2 x + 192 z y 2 + +192 sy 2 + 192 y 2 x − 1 92 y z 2 − 192 y s 2 − 192 y x 2 + 192 z x 2 + 192 s 2 x − 3 84 y sx = 0 . 5 4 The case of axisymmetri c e quation The equation (7) 2 ∂ 2 ∂ x∂ y f ( x, y , z , s ) + ∂ ∂ x f ( x, y , z , s ) ! ∂ 2 ∂ x 2 f ( x, y , z , s ) − ∆ f ( x, y , z , s ) = 0 , where ∆ = ∂ ∂ z 2 + ∂ ∂ s 2 , in p o lar co ordinat es s = r cos( φ ) , z = r sin ( φ ) tak es the form 2 ∂ 2 ∂ x∂ y f ( x, y , z ) + ∂ ∂ x f ( x, y , z ) ! ∂ 2 ∂ x 2 f ( x, y , z ) − ∂ 2 ∂ z 2 f ( x, y , z ) − ∂ ∂ z f ( x, y , z ) z = 0 (10) where we r eplace v ariable r on v ariable z After applying ( u, v )-transformation with v ( x, t, z ) = t ∂ ∂ t ω ( x, t, z ) − ω ( x, t, z ) , u ( x, t, z ) = ∂ ∂ t ω ( x, t, z ) the equation (10) takes the form − ∂ 2 ∂ t 2 ω ( x, t, z ) ! z t 2 ∂ ∂ x ω ( x, t, z ) ! ∂ 2 ∂ x 2 ω ( x, t, z ) + t 3 ∂ ∂ z ω ( x, t, z ) ! ∂ 2 ∂ t 2 ω ( x, t, z )+ + ∂ 2 ∂ t 2 ω ( x, t, z ) ! t 3 z ∂ 2 ∂ z 2 ω ( x, t, z ) − t 3 z ∂ 2 ∂ t∂ z ω ( x, t, z ) ! ∂ 2 ∂ z 2 ω ( x, t, z )+ + t 2 z ∂ ∂ z ω ( x, t, z ) ! ∂ 2 ∂ z 2 ω ( x, t, z ) + z t 2 ∂ 2 ∂ t∂ x ω ( x, t, z ) ! 2 ∂ ∂ x ω ( x, t, z ) − − 2 z t ∂ 2 ∂ t∂ x ω ( x, t, z ) ! ∂ ∂ x ω ( x, t, z ) ! 2 + z ∂ ∂ x ω ( x, t, z ) ! 3 + 2 z t ∂ ∂ x ω ( x, t, z ) − − 2 z t 2 ∂ 2 ∂ t∂ x ω ( x, t, z ) = 0 . This equation has solution of the form ω ( x, t, z ) = A ( x, z ) t + B ( t ) where function B ( t ) is arbitrary and the function A ( x, z ) satisfies the equation z ∂ ∂ x A ( x, z ) ! ∂ 2 ∂ x 2 A ( x, z ) − ∂ ∂ z A ( x, z ) − z ∂ 2 ∂ z 2 A ( x, z ) = 0 . (11) The solutions of the equation (11) can b e obtained with t he help of ( u, v )-transformatio n and a simplest of them has the form A ( x, z ) = C2 − C1 − C2 ln( C2 z ) − x. 6 Using the express ion ω ( x, t, z ) = A ( x, z ) t + B ( t ) with a giv en function A ( x, z ) and arbitrary function B ( t ) the solution of the equation (10) can be constructed. As example, in the case B ( t ) = ln ( t ) the elimination of the pa r ameter t from the r elat io ns f ( x, y , z ) t − t C2 + t C1 + t C2 ln( C2 z ) + tx − 1 = 0 , y − 1 + ln( t ) = 0 lead to the solution of the equation (1 0) f ( x, y , z ) = −  − e − y +1 C2 + e − y +1 C1 + e − y +1 C2 ln( C2 z ) + e − y +1 x − 1   e − y +1  − 1 . In the case B ( t ) = te t b y ana lo gy wa y w e find the solution f ( x, y , z ) = − C1 − C2 ln( C2 z ) − x + C2 + 1 / 2 y L amb ertW (1 / 2 √ y ) + +1 / 4 y  L amb ertW (1 / 2 √ y )  2 . The solution of the equation (11 ) A ( x, z ) = 2 / 9 x 3 z 2 lead to the function ω ( x, t, z ) = 2 / 9 x 3 t z 2 + B ( t ) where B ( t ) is arbitra ry function. In the case B ( t ) = ln( t ) w e find f ( x, y , z ) = 2 / 9 x 3 z 2 +  e − y +1  − 1 . In the case B ( t ) = t 2 + t − 2 w e get f ( x, y , z ) = 2 / 9  q 2 y + 2 √ y 2 + 12 √ y 2 + 12 + q 2 y + 2 √ y 2 + 12 y  x 3  y + √ y 2 + 12  q 2 y + 2 √ y 2 + 12 z 2 + +2 / 9 72 z 2 + 18 z 2 y 2 + 18 z 2 y √ y 2 + 12  y + √ y 2 + 12  q 2 y + 2 √ y 2 + 12 z 2 . 7 5 Ac kno wled gemen t This researc h w as partially supp orted b y the GRant 0 6 .01 CRF of HCSTD ASM and the RFBR Gran t References: 1. Xiaoping Xu, Stable-R ange Appr o ach to the Equation of Nonstationar y T r ansonic Gas flows , ArXiv: 0706.4 189 v1 , physics.flu-dyn, 28 Jun 2007, p. 1-19. 2. V. Dryuma, The Riema nn and E i nsten-Weyl ge ometries in the ory of differ ential e quations, their applic ations and al l that . A.B.Shabat et all.(eds.), New T rends in Inte grabilit y an d P artial S olv abilit y , Klu wer Academic Publishers, P r in ted in the Netherlands , 2004, p.115–156 . 3. Dryuma V.S., On solutions of t he he aven ly e quations and their gener alizations , ArXiv:gr- qc/0611001 v1 31 Oct 2006, p.1- 14. 3. Dryuma V.S., On dual e quation in the ory of the se c ond o r der OD E’s , ArXiv:nlin/0001047 v1 22 Jan 2007, p.1-17. 8

Original Paper

Loading high-quality paper...

Comments & Academic Discussion

Loading comments...

Leave a Comment