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Analysis of Oblique Shocks. P M V Subbarao Associate Professor Mechanical Engineering Department I I T Delhi. A Mild, Efficient and Compact Compressor …. Non Conical Inlets at Super Sonic Speeds. High Mach Number>x. Low Mach Number>x. High Angle Objects.
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Analysis of Oblique Shocks P M V Subbarao Associate Professor Mechanical Engineering Department I I T Delhi A Mild, Efficient and Compact Compressor ….
Non Conical Inlets at Super Sonic Speeds High Mach Number>x Low Mach Number>x
High Angle Objects Sleek Bodies at supersonic Speeds Bluff Bodies at supersonic Speeds
Mach Waves, Revisited • • A ‘’point-mass’’ object moving with Supersonic velocity Generates an infinitesimally weak “mach wave”. • The direction of flow remains unchanged across Mach wave.
Oblique Shock Wave • When generating object is larger than a “point”, shockwave is stronger than mach wave …. Oblique shock wave • -- shock angle • -- turning or “wedge angle”
Tangential Normal Ahead wx, Mtx ux, Mnx Of Shock Behind wy, Mty uy, Mny Shock Oblique Shock Wave Geometry Vx & Mx Vy & My uy & Mny wy & Mty ux & Mnx wx & Mtx Vy & My Vx & Mx • Shock is A CV & Must satisfy i) continuity ii) momentum iii) energy
æ ö - > - > ò ò r · = = - r + r ® r = r 0 V d s u A u A u u è ø x x y y x x y y . . C S Continuity Equation wy wx Vy Vx uy ux x y • For Steady Flow
• For Steady Flow w/o Body Forces ( ) - r + r = 0 u w A u w A x x x y y y r = r u u = w w x x y y x y Momentum Equation • Tangential Component Tangential velocity is Constant across oblique Shock wave • But from continuity
( ) - r + r = - ® 2 2 u A u A p p A x x y y y x + r = + r 2 2 p u p u x x x y y y • Normal Component Tangential velocity is Constant across oblique Shock wave
= + ® = + ® = 2 2 2 2 2 2 V u w V u w w w x x x x y y x y 2 2 u u 2 2 V V + = + x x h h x y + = + h h x x x y 2 2 2 2 Energy Equation • Write Velocity in terms of components • thus …
r = r u u x x y y b w x = w w x y b-q u + r = + r 2 2 p u p u x x x x y y y u w y y 2 2 u u b-q + = + x y c T c T q x y p p 2 2 Collected Oblique Shock Equations • Continuity • Momentum • Energy
Vx & Mx Vy & My • Defining: Mnx=Mxsin( Mtx=Mxcos( uy & Mny wy & Mty ux & Mnx wx & Mtx Vy & My • Then by similarity we can write the solution Vx & Mx
Letting • Similarity Solution Mnx= Mxsin(b)
Total Mach Number Downstream of Oblique Shock Tangential velocity is Constant across oblique Shock wave
Tangential velocity is Constant across oblique Shock wave
Tangential velocity is Constant across oblique Shock wave • Or … More simply .. If we consider geometric arguments
Oblique Shock Wave Angle • Properties across Oblique Shock wave ~ f(M1, b) • q is the geometric angle that “forces” the flow • How do we relateq to b
Oblique Shock Wave Angle (cont’d) • from Momentum
Oblique Shock Wave Angle (cont’d) • Solving for the ratio u2/u1 Implicit relationship for shock angle in terms of Free stream mach number and “wedge angle”
( ) ( ) ( ) é ù ( ) ( ) ( ) 2 2 b g + b - + g - b é ù é ù t a n 1 s i n 2 1 s i n M M ë û ë û ë û 1 1 ( ) q = t a n ( ) é ( ) ( ) ù ( ) ( ) ( ) 2 2 g + b + b + g - b é ù é ù 2 1 s i n t a n 2 1 s i n M M ë û ë û ë û 1 1 • Solve explicitly for tan(q)
Oblique Shock Wave Angle (cont’d) • Simplify Numerator
Oblique Shock Wave Angle (cont’d) • Collect terms • “Wedge Angle” Given explicitly as function of shock angle and freestream Mach number • Two Solutions “weak” and “strong” shock wave. In reality weak shock typically occurs; strong only occurs under very Specialized circumstances .e.g near stagnation point for a detached Shock.
“strong shock” M1=5.0 “weak shock” max curve M1=4.0 Oblique Shock Wave Angle M1=3.0 M1=2.5 M1=1.5 M1=2.0
High Angle Objects q <qmax q >qmax
Solving for Oblique Shock Wave Angle in Terms of Wedge Angle • As derived • “Wedge Angle” Given explicitly as function of shock angle and freestream Mach number • For most practical applications, the geometric deflection angle (wedge angle) and Mach number are prescribed .. Need in terms of and M1 • Obvious Approach …. Numerical Solutionusing Newton’s method
Solving for Oblique Shock Wave Angle in Terms of Wedge Angle (cont’d) • Newton method
Solving for Oblique Shock Wave Angle in Terms of Wedge Angle (cont’d) • Newton method (continued) • Iterate until convergence
Solving for Oblique Shock Wave Angle in Terms of Wedge Angle (cont’d) Increasing Mach • “Flat spot” Causes potential Convergence Problems with Newton Method
Solving for Oblique Shock Wave Angle in Terms of Wedge Angle (cont’d) • Newton method … Convergence can often be slow (because of low derivative slope) • Converged solution
Solving for Oblique Shock Wave Angle in Terms of Wedge Angle (concluded) • Newton method … or can “toggle” to strong shock solution • Strong shock solution
Solving for Oblique Shock Wave Angle in Terms of Wedge Angle (improved solution) • Because of the slow convergence of Newton’s method for this implicit function… explicit solution … (if possible) .. Or better behaved .. Method very desirable Substitute
Solving for Oblique Shock Wave Angle in Terms of Wedge Angle (improved solution)(cont’d) • But, since
Solving for Oblique Shock Wave Angle in Terms of Wedge Angle (improved solution)(cont’d) • Simplify and collect terms
Solving for Oblique Shock Wave Angle in Terms of Wedge Angle (improved solution)(cont’d) • Again, Since
Solving for Oblique Shock Wave Angle in Terms of Wedge Angle (improved solution)(cont’d) • Regroup and collect terms
Solving for Oblique Shock Wave Angle in Terms of Wedge Angle (improved solution)(cont’d) • Finally • Regrouping in terms of powers of tan()
Solving for Oblique Shock Wave Angle in Terms of Wedge Angle (improved solution)(cont’d) • Letting • Result is a cubic equation of the form • Polynomial has 3 real roots i) weak shock ii) strong shock iii) meaningless solution ( < 0)
Solving for Oblique Shock Wave Angle in Terms of Wedge Angle (improved solution)(cont’d) • Numerical Solution of Cubic (Newton’s method)
Solving for Oblique Shock Wave Angle in Terms of Wedge Angle (improved solution)(cont’d) • Collecting terms
Solving for Oblique Shock Wave Angle in Terms of Wedge Angle (improved solution)(cont’d) • Solution Algorithm (iterate to convergence) • Where again
Solving for Oblique Shock Wave Angle in Terms of Wedge Angle (improved solution)(cont’d) • Properties of Solver algorithm are much improved Original Algorithm Improved Algorithm • Improved algorithm • Original algorithm
Solving for Oblique Shock Wave Angle in Terms of Wedge Angle (improved solution)(cont’d) • Three Solutions always returned depending on start condition Original Algorithm • Weak Shock Solution Improved Algorithm
Solving for Oblique Shock Wave Angle in Terms of Wedge Angle (improved solution)(cont’d) • Three Solutions always returned depending on start condition Improved Algorithm • Strong Shock Solution