The measurements of part V (reference 1) of this series of reports, which concerned comparatively long ring profiles, are supplemented by measurements on shorter rings as they are used for shrouded propellers and cowlings of ring-shaped radiators. Mass-flow coefficients and profile drags are given. Furthermore, it has to be determined how far the potential theory describes the flow phenomenon with sufficient accuracy and whether the present theory for the calculation of thin annular profile yields useful profile forms and is suitable for determination of the mass flow for thick profiles.Translated from Zentrale fuer Wissenschaftliches Berichtswesen der Luftfahrtforschung des Generalluftzeugmeisters (ZWB), Berlin-Adlershof, Forschungsbericht...
Axial forces were measured on five cylinders at M = 5 for Re = 4,000,000/ft and 37,000,000/ft. The p...
The results indicate that for Mach numbers up to 0.60 the upwash angles can be predicted accurately ...
'The views expressed herein are those of the authors alone and do not neeessurily represent tho...
The measurements of part V (reference 1) of this series of reports, which concerned comparatively lo...
It is shown how one may obtain, in a simple manner, the forms of ring-shaped bodies from existing ta...
The dependence of the maximum incremental velocities and air forces on a circular cowling on the mas...
The present report presents as a supplement to the fourth report (FB 1236/4) in the series of invest...
The investigations carried out in a previous report (NACA TM 1325) concerning the flow about ring-sh...
The variation in the drag coefficient for low-Reynolds-number flow past rings orient-ated normal to ...
For application in practice for annular radiator fairings and similar arrangements, two new classes ...
"It is shown how one may obtain, in a simple manner, the forms of ring-shaped bodies from existing t...
The article considers the method of improving the characteristics of the ring inlet device, taking i...
The mounting of either a tractor or pusher propeller near a streamlined wing not only affects the ef...
This report gives the results of measurements of the lift, drag, and propeller characteristics of se...
The contribution deals with numerical modelling of flow through the shaft labyrinth seal for various...
Axial forces were measured on five cylinders at M = 5 for Re = 4,000,000/ft and 37,000,000/ft. The p...
The results indicate that for Mach numbers up to 0.60 the upwash angles can be predicted accurately ...
'The views expressed herein are those of the authors alone and do not neeessurily represent tho...
The measurements of part V (reference 1) of this series of reports, which concerned comparatively lo...
It is shown how one may obtain, in a simple manner, the forms of ring-shaped bodies from existing ta...
The dependence of the maximum incremental velocities and air forces on a circular cowling on the mas...
The present report presents as a supplement to the fourth report (FB 1236/4) in the series of invest...
The investigations carried out in a previous report (NACA TM 1325) concerning the flow about ring-sh...
The variation in the drag coefficient for low-Reynolds-number flow past rings orient-ated normal to ...
For application in practice for annular radiator fairings and similar arrangements, two new classes ...
"It is shown how one may obtain, in a simple manner, the forms of ring-shaped bodies from existing t...
The article considers the method of improving the characteristics of the ring inlet device, taking i...
The mounting of either a tractor or pusher propeller near a streamlined wing not only affects the ef...
This report gives the results of measurements of the lift, drag, and propeller characteristics of se...
The contribution deals with numerical modelling of flow through the shaft labyrinth seal for various...
Axial forces were measured on five cylinders at M = 5 for Re = 4,000,000/ft and 37,000,000/ft. The p...
The results indicate that for Mach numbers up to 0.60 the upwash angles can be predicted accurately ...
'The views expressed herein are those of the authors alone and do not neeessurily represent tho...