Accession Number : AD0477906


Title :   PRELIMINARY FLIGHT TEST DATA. UH-1B HIGH PERFORMANCE HELICOPTER WITH AUXILIARY PROPULSION


Descriptive Note : Technical Report


Corporate Author : ARMY TRANSPORTATION RESEARCH COMMAND FORT EUSTIS VA FORT EUSTIS United States


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/477906.pdf


Report Date : 01 Feb 1964


Pagination or Media Count : 30


Abstract : The following pages present some of the previous flight test results achieved with the high performance UH1B helicopter operating as a pure helicopter and in a winged configuration.


Descriptors :   HELICOPTERS , FLIGHT TESTING , PERFORMANCE(ENGINEERING) , VELOCITY , VIBRATION , THRUST , PITCH(MOTION) , STABILITY


Distribution Statement : APPROVED FOR PUBLIC RELEASE