An investigation of the suitability of the N.A.C.A. Roots type aircraft engine supercharger to flight-operating conditions, as determined the effects of the use of the supercharger upon engine operation and airplane performance, is described in this report. Attention was concentrated on the operation of the engine-supercharger unit and on the improvement of climbing ability; some information concerning high speeds at altitude was obtained. The supercharger was found to be satisfactory under flight-operating conditions. Although two failures occurred during the tests, the causes of both were minor and have been eliminated. Careful examination of the engines revealed no detrimental effects which could be attributed to supercharging. Marked im...
The investigation described in this report was conducted for the purpose of comparing an oleo-rubber...
This report presents the results of flight tests with three different airplanes using several types ...
This report gives the results of the tests of seven 2 by 12 foot airfoils (Clark Y, smooth and corru...
This report describes a roots type aircraft engine supercharger and presents the results of some tes...
This report presents the results of an investigation to determine the effect of different supercharg...
This report presents the comparative flight results of a roots supercharger and a turbocentrifugal s...
This report presents the results of preliminary tests made on the effects of supercharging an air-co...
This report presents the results of tests made on three sizes of roots type aircraft engine supercha...
An investigation of the suitability of the N.A.C.A. Roots type aircraft engine supercharger to fligh...
This investigation was made to determine the pressure distribution over a rib of the wing and over a...
Several investigations have been made on single-cylinder test engines to determine the performance c...
.kn investigation of hhe suitability of the X. A. C..4. Roots type aircraft erigitte super-charger t...
Fundamental investigations of compressibility phenomena for airfoils have shown that serious adverse...
At the request of the Army Air Corps, an investigation of the pressure distribution over PW-9 wing m...
Discussed here are the principles and operation of aircraft engine superchargers used to maintain an...
The investigation described in this report was conducted for the purpose of comparing an oleo-rubber...
This report presents the results of flight tests with three different airplanes using several types ...
This report gives the results of the tests of seven 2 by 12 foot airfoils (Clark Y, smooth and corru...
This report describes a roots type aircraft engine supercharger and presents the results of some tes...
This report presents the results of an investigation to determine the effect of different supercharg...
This report presents the comparative flight results of a roots supercharger and a turbocentrifugal s...
This report presents the results of preliminary tests made on the effects of supercharging an air-co...
This report presents the results of tests made on three sizes of roots type aircraft engine supercha...
An investigation of the suitability of the N.A.C.A. Roots type aircraft engine supercharger to fligh...
This investigation was made to determine the pressure distribution over a rib of the wing and over a...
Several investigations have been made on single-cylinder test engines to determine the performance c...
.kn investigation of hhe suitability of the X. A. C..4. Roots type aircraft erigitte super-charger t...
Fundamental investigations of compressibility phenomena for airfoils have shown that serious adverse...
At the request of the Army Air Corps, an investigation of the pressure distribution over PW-9 wing m...
Discussed here are the principles and operation of aircraft engine superchargers used to maintain an...
The investigation described in this report was conducted for the purpose of comparing an oleo-rubber...
This report presents the results of flight tests with three different airplanes using several types ...
This report gives the results of the tests of seven 2 by 12 foot airfoils (Clark Y, smooth and corru...