Universal single level implicit algorithm for gasdynamics

Lombard, C. K.; Venkatapathy, Ethiraj; Bardina, Jorge

doi:10.2514/6.1984-1533

Cited by 12 publications

(2 citation statements)

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“….An alternative approach that has been used by several investigators [4][5][6][7][8][9][10][11][12][13][14], is to modify a NS code so that it can space march the solution in supersonic regions. The drawback to this approach is that the NS equations are usually iterated several times at each streamwise step as the solution is marched downstream.…”

Section: Introductionmentioning

confidence: 99%

PNS algorithm for solving supersonic flows with upstream influences

Miller

Tannehill

Lawrence

1998

36th AIAA Aerospace Sciences Meeting and Exhibit

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Section: Introductionmentioning

confidence: 99%

PNS algorithm for solving supersonic flows with upstream influences

Miller

Tannehill

Lawrence

1998

36th AIAA Aerospace Sciences Meeting and Exhibit

View full text Add to dashboard Cite

show abstract

Section: Introductionmentioning

confidence: 99%

PNS algorithm for solving supersonic flows with upstream influences

Miller

View full text Add to dashboard Cite

The qualiQr of this reproduction b dependent upon the quality of the copy submitted. Broken or indistinct print, colored or poor quality illustrations and photographs, print bleedthrough, substandard margins, and improper alignment can adverse^ afifect reproduction. In the unlikely event that the author did not send UMI a complete manuscript and there are missing pages, these will be noted. Also, if unauthorized copyright material had to be removed, a note will indicate the deletioiL Oversize materials (e.g., maps, drawings, charts) are reproduced by sectioning the original, b^inning at the upper left-hand comer and continuing from left to right in equal sections with small overijq)s. Each original is also photographed in one exposure and is included in reduced form at the back of the book.

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