C.P. No. 985 MINISTRY OF TECHNOLOGY AERONAUTICAL RESEARCH COUNCIL Measurements of Pressure Fluctuations and Skin Friction on the Upper Surface of a Slender
نویسندگان
چکیده
SuNihiiAIly FOUr slW~%%-~ing free-fligh t models were used to invcstigato the local pressure fluctuatmns, skin-fricticn and static-prcssurcs across OM spanwise station unaer ver37ing coalitions of lift ma ?,isch number. At Nach numbers bctneen 0.8 ana l-2 a dell-estzblishcd free-vortex flow ~ss a~hiaved over the uppzr surface. T%e intention nas to deternine the ratlo between the intcnsiti~ 3f tho pressdw fYdcD2,tions and the 10231 sldn-friction under conditions of atthea and scpsraied flows. While ncasurenonts of masonable quality were obtained, the inherent limitations of the tclmetry sys2-e~ did not allow a sufficiently broad. band of pressure-fluctuaclon frequenmes to be masured so that the relationship i;ith skin-friction could not be determine& Therefore, 3. detailed analysis of the results ana comparlaon with other expetimental OS theoretical aats has not been attenpted. But the present results are consIdered to be a useful and signlf~cant addition to the rather nertgre experinental data that exists on this subject, partmdsrly because they were obtamea in con&itions free from flow imperfactzons suck as free-stream turbulence which exist in most wind-tunnels.
منابع مشابه
C.P. No. IO18 MINISTRY OF TECHNOLOGY AERONAUTICAL RESEARCH COUI’KX CURRENT PAPERS Measurements of the Effects of Thickness on Vortex Breakdown Position on a Series of Sharp-Edged Delta Wings
متن کامل
C.P. No. 625 MINISTRY OF AVIATION AERONAUTICAL RESEARCH COUNCIL CURRENT PAPERS Notes on some Experimental and Theoretical Results for the Boundary Layer Development aft of the Shock in a Shock-Tube BY LONDON: HER MAJESTY’S STATIONERY OFFICE 1963 SIX SHILLINGS NET
متن کامل
C.P. No. 1294 PROCUREMENT EXECUTIVE, MINISTRY OF DEFENCE AERONAUTICAL RESEARCH COUNCIL CURRENT PAPERS SLR Temperature Measurements in the Supersonic Expansion of Nitrogen in a Shock-Tunnel bY
SUMMARY Temperature measurements, using the SLR method, are presented for the expansion of nitrogen in nozzles attached to a shock-tube. The measurements were made at an area ratio of 8.5 in a two-dimensional nozzle and at an area ratio of 152 in a conical nozzle. Initial conditions were such that at the entrance to the nozzles the temperature ranged between about 2500 K and 5300 K and the pres...
متن کاملThe Analytic Technique and Experimental Research Methods of Post-buckling about Slender Rod Strings in Wellbore
The buckling behavior of rod strings in wellbore is one of the key issues in petroleum engineering. The slender rod strings in vertical wellbore were selected as research objects. Based on the energy method, the critical load formulas of sinusoidal and helical buckling were derived for the string with the bottom of the wellbore pressure. According to the sinusoidal and helical buckling’s geomet...
متن کاملC.P. No. i335 PROCUREMENT EXECUTIVE, MINISTRY OF DEFENCE AERONAUTICAL RESEARCH COUNCIL CURRENT PAPERS Measurements of Secondary Loss in a Model Turbine with Variable Inlet Boundary Layer
SUMMARY Detailed measurements have been made of the casing boundary layer flow before and after the nozzle blades of a single stage model air turbine. The measurements were made with the natural casing inlet boundary layer and two artificially thickened boundary layers. The results differ considerably from those usually obtained in two dimensional cascades. There was no sign of the usual second...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
عنوان ژورنال:
دوره شماره
صفحات -
تاریخ انتشار 1966