Numerical Calculations of the Transonic Flow Past a Swept Wing
Numerical Calculations of the Transonic Flow Past a Swept Wing
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In our eReader you can find the full English version of the book. Read Numerical Calculations of the Transonic Flow Past a Swept Wing Online - link to read the book on full screen. Our eReader also allows you to upload and read Pdf, Txt, ePub and fb2 books. In the Mini eReder on the page below you can quickly view all pages of the book - Read Book Numerical Calculations of the Transonic Flow Past a Swept Wing
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To quickly assess the difficulty of the text, read a short excerpt:
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.
What to read after Numerical Calculations of the Transonic Flow Past a Swept Wing?
You can find similar books in the "Read Also" column, or choose other free books by Antony Jameson to read onlineMoreLess
To quickly assess the difficulty of the text, read a short excerpt:
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.
What to read after Numerical Calculations of the Transonic Flow Past a Swept Wing?
You can find similar books in the "Read Also" column, or choose other free books by Antony Jameson to read onlineMoreLess
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