Computation of the Transonic Flow About a Swept Wing in the Presence of An Engin
Computation of the Transonic Flow About a Swept Wing in the Presence of An Engin
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In our eReader you can find the full English version of the book. Read Computation of the Transonic Flow About a Swept Wing in the Presence of An Engin 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 Computation of the Transonic Flow About a Swept Wing in the Presence of An Engin
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To quickly assess the difficulty of the text, read a short excerpt:
5»(Y1+YM1) DYO- ( SHRY- 1 . ) ♦ . 5/SQRT ( 1 -Y0»»2 ) •♦3 CALL SHRNCMP ( JA, JB, DY, YSHRNK, DYO ) DZ0>SHP. Z-1 .
CALL SHRNCMP (KA, KB, DZ, ZSHRNK, DZO ) DD—RX-DX DO 10 I>1, MX DD«DD>DX IF (ABS(OO) . LE. XMAX) THEN D0«OD D1-1. D2«0. ELSE IF (DD. LT. O. ) THEN B—1.
- Ill - ELSE B>1 EK0I7 A«1. -( (D0-B*XMAZ)/(1. -ZMAZ}}«*2 C>SQRT(A) O0*B*XMAZ-i- ( DD-B*XMAZ ) /C 01»A«C 02»-(DD-B*XMAZ)*3. /(A*( 1 . -ZMAZ)**2) END IF AO(I}»DO A1(I)». 5*D1/DX A2(I)»D1»D1 A3(I)a. 5*DZ*02 10 CONTINUE DDaRY DO 20 J-2, ...Ky DDaDD-DY A»1. -DD»DD C«SQRT(A} 17 (ABS(DO-YSHIUnC(3)}. GB. YSHRNK(4} ) THEN D1>2. *A*C B0( J)>. 5*DD/C B1( J)». 5»D1/DY B2(J)>D1*D1*V2 B3 ( J ) ■- 1 . 5*DD*DY/A ELSE CALL SHRINK ( YSHRNK, DD, DO, 01, 02) 01«1. /(D1+. 5/{A»C)) D2—D 1 ♦ ( 02+ 1 . 5*DD/ ( A*A*C ) ) B0(J)»D0+. 5»DD/C B1(J)«. 5»D1/DY B2(J)»V2»D1»D1 B3(J)». 5*OY*02 END IF 20 CONTINUE 00«-DZ-OZ-ZO DO 30 K>2, K2 DD>DD-fOZ IF (ABS(OD) . LE. ZMAZ) THEN IF (ABS(DD-ZSHRNK(3) } . GE. ZSHRNK(4} ) THEN DO'DO 01-1.
What to read after Computation of the Transonic Flow About a Swept Wing in the Presence of An Engin?
You can find similar books in the "Read Also" column, or choose other free books by David S Ross to read onlineMoreLess
To quickly assess the difficulty of the text, read a short excerpt:
5»(Y1+YM1) DYO- ( SHRY- 1 . ) ♦ . 5/SQRT ( 1 -Y0»»2 ) •♦3 CALL SHRNCMP ( JA, JB, DY, YSHRNK, DYO ) DZ0>SHP. Z-1 .
CALL SHRNCMP (KA, KB, DZ, ZSHRNK, DZO ) DD—RX-DX DO 10 I>1, MX DD«DD>DX IF (ABS(OO) . LE. XMAX) THEN D0«OD D1-1. D2«0. ELSE IF (DD. LT. O. ) THEN B—1.
- Ill - ELSE B>1 EK0I7 A«1. -( (D0-B*XMAZ)/(1. -ZMAZ}}«*2 C>SQRT(A) O0*B*XMAZ-i- ( DD-B*XMAZ ) /C 01»A«C 02»-(DD-B*XMAZ)*3. /(A*( 1 . -ZMAZ)**2) END IF AO(I}»DO A1(I)». 5*D1/DX A2(I)»D1»D1 A3(I)a. 5*DZ*02 10 CONTINUE DDaRY DO 20 J-2, ...Ky DDaDD-DY A»1. -DD»DD C«SQRT(A} 17 (ABS(DO-YSHIUnC(3)}. GB. YSHRNK(4} ) THEN D1>2. *A*C B0( J)>. 5*DD/C B1( J)». 5»D1/DY B2(J)>D1*D1*V2 B3 ( J ) ■- 1 . 5*DD*DY/A ELSE CALL SHRINK ( YSHRNK, DD, DO, 01, 02) 01«1. /(D1+. 5/{A»C)) D2—D 1 ♦ ( 02+ 1 . 5*DD/ ( A*A*C ) ) B0(J)»D0+. 5»DD/C B1(J)«. 5»D1/DY B2(J)»V2»D1»D1 B3(J)». 5*OY*02 END IF 20 CONTINUE 00«-DZ-OZ-ZO DO 30 K>2, K2 DD>DD-fOZ IF (ABS(OD) . LE. ZMAZ) THEN IF (ABS(DD-ZSHRNK(3) } . GE. ZSHRNK(4} ) THEN DO'DO 01-1.
What to read after Computation of the Transonic Flow About a Swept Wing in the Presence of An Engin?
You can find similar books in the "Read Also" column, or choose other free books by David S Ross to read onlineMoreLess
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