Add to ORKGThe influence of thickness and length of a hub projecting from an inlet opening was investigated on one of the two new classes of circular cowls reported in NACA TM 1360
Exploratory tests of a circular internal-contraction inlet were made at Mach numbers of 2.00 and 2.3...
Concepts are investigated for obtaining both low cowl drag and good inlet performance at high angles...
Mass flux measurements associated with chocked flows through four Borda type inlet geometries: circu...
For application in practice for annular radiator fairings and similar arrangements, two new classes ...
The dependence of the maximum incremental velocities and air forces on a circular cowling on the mas...
The investigations carried out in a previous report (NACA TM 1325) concerning the flow about ring-sh...
The development of new cowlings, applicable to a short-nose radial engine, is described. These cowli...
It is shown how one may obtain, in a simple manner, the forms of ring-shaped bodies from existing ta...
"The influence of thickness and length of a hub projecting from an inlet opening was investigated on...
The present report presents as a supplement to the fourth report (FB 1236/4) in the series of invest...
Data are presented of the flow conditions in the vicinity of an NACA D sub S -type cowling. Tests we...
Pressure distributions on three inlets having different cowl lengths were obtained in the Langley 16...
An extensive series of wind-tunnel tests on a half-scale conventional, nacelle model were made by th...
The measurements of part V (reference 1) of this series of reports, which concerned comparatively lo...
The results of a theoretical investigation of geometric variables for lift-cruise-fan, tilting nacel...
Exploratory tests of a circular internal-contraction inlet were made at Mach numbers of 2.00 and 2.3...
Concepts are investigated for obtaining both low cowl drag and good inlet performance at high angles...
Mass flux measurements associated with chocked flows through four Borda type inlet geometries: circu...
For application in practice for annular radiator fairings and similar arrangements, two new classes ...
The dependence of the maximum incremental velocities and air forces on a circular cowling on the mas...
The investigations carried out in a previous report (NACA TM 1325) concerning the flow about ring-sh...
The development of new cowlings, applicable to a short-nose radial engine, is described. These cowli...
It is shown how one may obtain, in a simple manner, the forms of ring-shaped bodies from existing ta...
"The influence of thickness and length of a hub projecting from an inlet opening was investigated on...
The present report presents as a supplement to the fourth report (FB 1236/4) in the series of invest...
Data are presented of the flow conditions in the vicinity of an NACA D sub S -type cowling. Tests we...
Pressure distributions on three inlets having different cowl lengths were obtained in the Langley 16...
An extensive series of wind-tunnel tests on a half-scale conventional, nacelle model were made by th...
The measurements of part V (reference 1) of this series of reports, which concerned comparatively lo...
The results of a theoretical investigation of geometric variables for lift-cruise-fan, tilting nacel...
Exploratory tests of a circular internal-contraction inlet were made at Mach numbers of 2.00 and 2.3...
Concepts are investigated for obtaining both low cowl drag and good inlet performance at high angles...
Mass flux measurements associated with chocked flows through four Borda type inlet geometries: circu...