Results of flight tests of the performance and cooling characteristics of three NACA D cowlings and of a conventional NACA D cowling on the XP-42 airplane are summarized and compared. The D cowling is, in general, characterized by the use of an annular inlet and diffuser section for the engine-cooling air. The D cowlings tested were a long-nose high-inlet-velocity cowling, a short-nose high-inlet-velocity cowling, and a short-nose low inlet-velocity cowling. The use of wide-chord propeller cuffs or an axial-flow fan with the D cowlings increased the cooling pressure recoveries in the climb condition at the expense of some of the improvement in speed
Typical models and the testing technique used in the NACA free-spinning wind tunnel are described in...
Report presents the results of an investigation of full-scale nose-slot cowlings conducted in the NA...
Report presents the results of tests of longitudinal stability characteristics of models of several ...
An extended experimental study has been made in regard to the various refinements in the design of e...
A comprehensive investigation has been carried on with full-scale models in the NACA 20-foot wind tu...
Results of flight tests of the performance and cooling characteristics of three NACA D cowlings and ...
This report presents the results of flight tests with three different airplanes using several types ...
An investigation was conducted in the NACA full-scale wind tunnel to determine the drag and the prop...
The drag characteristics of eight radial-engine cowlings have been determined over a wide speed rang...
Report presents the results of tests conducted on 28 wing-fuselage combinations made in the variable...
Report presents the results of an investigation of the general aerodynamic characteristics of the NA...
Data are presented of the flow conditions in the vicinity of an NACA D sub S -type cowling. Tests we...
This report is the fifth of a series giving the results obtained from wind tunnel tests on the inter...
This report describes the 5-inch bore by 7-inch stroke single cylinder test engine used at the Langl...
This report gives the results of the second portion of an investigation in the twenty-foot Propeller...
Typical models and the testing technique used in the NACA free-spinning wind tunnel are described in...
Report presents the results of an investigation of full-scale nose-slot cowlings conducted in the NA...
Report presents the results of tests of longitudinal stability characteristics of models of several ...
An extended experimental study has been made in regard to the various refinements in the design of e...
A comprehensive investigation has been carried on with full-scale models in the NACA 20-foot wind tu...
Results of flight tests of the performance and cooling characteristics of three NACA D cowlings and ...
This report presents the results of flight tests with three different airplanes using several types ...
An investigation was conducted in the NACA full-scale wind tunnel to determine the drag and the prop...
The drag characteristics of eight radial-engine cowlings have been determined over a wide speed rang...
Report presents the results of tests conducted on 28 wing-fuselage combinations made in the variable...
Report presents the results of an investigation of the general aerodynamic characteristics of the NA...
Data are presented of the flow conditions in the vicinity of an NACA D sub S -type cowling. Tests we...
This report is the fifth of a series giving the results obtained from wind tunnel tests on the inter...
This report describes the 5-inch bore by 7-inch stroke single cylinder test engine used at the Langl...
This report gives the results of the second portion of an investigation in the twenty-foot Propeller...
Typical models and the testing technique used in the NACA free-spinning wind tunnel are described in...
Report presents the results of an investigation of full-scale nose-slot cowlings conducted in the NA...
Report presents the results of tests of longitudinal stability characteristics of models of several ...