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Linearized flow past a flat plate

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13 larger stretching function would yield a more correct BL thickness and a less correct wall shear stress, while a smaller…
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14 APPENDIX I SOLUTIONS FOR A GENERAL CLASS OF BOUNDARY LAYER PROBLEMS Let us consider the class of incompressible steady…
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15 have more than one inflection point and a local velocity within the BL which may exceed the free stream velocity or the…
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16 APPENDIX II EXACT SOLUTION OF THE BOUNDARY LAYER EQUATIONS FOR THE UIV CASE The exact solution of equation 1 with uo(y…
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REFERENCES 1. Ernst, W.D., "Recircu1atory Flow in a Cylindrical Cavity," Rensselaer Polytechnic Institute Tech.…
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4· k o J.3 1.2 k 1./ 18 Fig. 2a von ~iscs Stretching Function for U ~ If C Fig. 2b ~ises Stretching Function for…
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.3 ~ra; --pw V-:o .2. . I 19 !"ig. 3a Wall SheRr Stress for U ~ Uc
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20 UjUc fig. 3b Wall Shear Stress for Dc ~ U
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2. I .. ., " r " r1 :1 r' ., :1 r. ., ., n n 1J n r. r l:fExact o SFL (von Mises) + SFL (Oseen…
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4.~ I I I i :3.~ I 2. - /. I )1 Exact o SFL (von Mises) -t- SFL (Oseen) .2 4 Fig. MlU .b SFL Boundary Layer…
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5.- 4 . .3. 2. /. ~ Exact o SFL (von Mises) + SFL (Oseen) I .2 --~4-'-"--- uju Fig. 4c ! ."b • .…

Modes of aerodynamic suspension for high-speed land vehicles

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TR AE 6809 FINAL SU~~Y REPORT ON RESEARCH PERFORMED UNDER RESEARCH GRANT NSF-GK- 6l8 Prepared for the National Science…
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TR AE 6809 FINAL SUMMARY REPORT ON RESEARCH PERFORMED UNDER RESEARCH GRANT NSF-GK-618 Prepared for the National Science…
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ABSTRACT FINAL SUMMARY REPORT ON RESEARCH PERFORMED UNDER RESEARCH GRANT NSF-GK 618 MODES OF AERODYNAMIC SUSPENSION FOR…
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- 2 - SUMMARY OF RESEARCHES A general survey of the problem studied under this grant and of the related problems of Project…
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- 3 - jet curtain that is deflected to the rear is analyzed with consideration of the viscous effects of the moving ground.…
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- 4 - changes. Unfortunately, because of the assumptions that had to be made to make the analyses manageable, results have…
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- 5 - conditions of a ground-effect support device in forward motion. A view of this experimental rig is shown in Fig. 6.…
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- 6 - Mark Ia was the first model to be flight tested, but in the initial attempt the propulsion engine stopped almost…
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- 7 - has been designed by Mr. D. H. Dennis (who, having been the first to advocate its use in tube vehicles, has been…
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- 8 - LIST OF PUBLICATIONS Foa, J.V., "High-Speed Transport in Nonevacuated Tubes," 1966 National Transportation…
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- 9 - PARTICIPATING PERSONNEL Participating in this project have been six doctoral students (z. Chang, G. Cooke, C. Sun, W.…
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FIG. 1
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FIG. 2 FIG. 3
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FIG. 4 FIG.5
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