Numerical Calculations of the Transonic Flow Past a Swept Wing

Cover Numerical Calculations of the Transonic Flow Past a Swept Wing
Numerical Calculations of the Transonic Flow Past a Swept Wing
Antony Jameson
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LE. NC) GC TO 11 ZO • . 5*(Zb(l) ♦ZSINO) IF (KSYM, Ne. 3) ZO « Zi)(i) DQ 62 K=1, NC 62 ZS(K) - Zi(K) -ZO ZTIP « ZS(NC) RETURN f>0C FuR. -iATdX) 59 510 FC»tM*T(8F10. 6) 600 FURMATdHl) 610 F0RMAT(Fli. A, 7Fli).^) S03RCUTlNt COCFD 1 2 (KS SfcTS U DirlbNS DX DY KY DZ ZC Kl K2 IF DZ Zt Kl K2 AX AY AZ BX bl XMAX zriAx SY SCAL i>CALZ V2 Wl W2 S73 BBX ABX CBX A6BX DC DD B IF A AS C DC Dl 12 (AE P STRFTCHt ION ACCl Z(l) « 2. /N « i. /t « NY » 2. /N ■ 1.
m 1 » NZ YM. TQ. O) G ■ l. /N • '). = 3 m N|Z - .
...;> « *i • 0. = 0.
■ . 62t = . 625 ■ . 5 « XT£C - ZTIF = (DX/ » SCAL « ( Wl* « SORT = -tJX* - 1. - «= ( l**.
• 4BX SORT I=2»NX » ( I = 1.
S(OD). GT. X " C6X = SORT ■ ABXf = ABX* » 4S/C (NX#NY#NZ»KSYf*XT-0, ZTIP*XnAX»ZMAX# SY»bCAL»SCALZ»AX>AY»AZ, AO»Al, A2, A3, bO»Bi, b<: cl="" c3="" pakatjolk="" and="" spasxisc="" cjokclnatts="" al="" a2="" l="">C2(i), C3 (1) )» fZ X Y ♦ 1 Z -D TO 1 Z ♦ 2 /( . ECCjl+KMAX + XMAX) /(i. F O00ol*Z»'/iX ) DY)**2 /SCALZ QX/CZ)**^ (73.


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