On Supersonic Compressors And Nozzles Supplement to Amp Report 821r
On Supersonic Compressors And Nozzles Supplement to Amp Report 821r
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In our eReader you can find the full English version of the book. Read On Supersonic Compressors And Nozzles Supplement to Amp Report 821r 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 On Supersonic Compressors And Nozzles Supplement to Amp Report 821r
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To quickly assess the difficulty of the text, read a short excerpt:
6 is not quite certain.
Each of the streamlines shown in the figijre may serve as a nozzle contour. For the purpose of comparison these different streamlines were so magnified that they correspond to the same throat diameter and then superim- posed. The result is shown in Table III, The coordinates of points on these contours corresponding to throat, transition, and exit are given in Table IV; R being the radius of curvature at the throat. The contour correspond- ing to 77 =, 1 is omitted becau...se it would be too long; even the contour t^ = . 2 is rather long. It appears reasonable to employ the line 7^ = . 5 for design. (The line 77 =, 6 is not much shorter and its location is uncertain. ) The contoior 97 = . 5 yields a length of 2, 5 throat diameters between throat and exit, a length which appears rather acceptable.
As to the details of the calculation, the following may be mentioned. The basic flow F^ was chosen as one whose streamlines are essentially hyperbolas; more exactly h =/l+|^ in the terminology of Part I of the previous report.
What to read after On Supersonic Compressors And Nozzles Supplement to Amp Report 821r?
You can find similar books in the "Read Also" column, or choose other free books by Kurt Otto Friedrichs to read onlineMoreLess
To quickly assess the difficulty of the text, read a short excerpt:
6 is not quite certain.
Each of the streamlines shown in the figijre may serve as a nozzle contour. For the purpose of comparison these different streamlines were so magnified that they correspond to the same throat diameter and then superim- posed. The result is shown in Table III, The coordinates of points on these contours corresponding to throat, transition, and exit are given in Table IV; R being the radius of curvature at the throat. The contour correspond- ing to 77 =, 1 is omitted becau...se it would be too long; even the contour t^ = . 2 is rather long. It appears reasonable to employ the line 7^ = . 5 for design. (The line 77 =, 6 is not much shorter and its location is uncertain. ) The contoior 97 = . 5 yields a length of 2, 5 throat diameters between throat and exit, a length which appears rather acceptable.
As to the details of the calculation, the following may be mentioned. The basic flow F^ was chosen as one whose streamlines are essentially hyperbolas; more exactly h =/l+|^ in the terminology of Part I of the previous report.
What to read after On Supersonic Compressors And Nozzles Supplement to Amp Report 821r?
You can find similar books in the "Read Also" column, or choose other free books by Kurt Otto Friedrichs to read onlineMoreLess
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