Accession Number : AD0092212


Title :   FREE-FLIGHT INVESTIGATION OF THE CONTROL EFFECTIVENESS OF A DIFFERENTIALLY DEFLECTED HORIZONTAL TAIL AT MACH NUMBERS FROM 0.8 TO 1.6


Descriptive Note : Research memo.


Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA


Personal Author(s) : Mitchell, Jesse L ; Vitale, A James


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/092212.pdf


Report Date : 26 Apr 1956


Pagination or Media Count : 28


Descriptors :   *ROLL , *HORIZONTAL STABILIZERS , *ROCKET MODELS , TAIL ASSEMBLIES , TRANSONIC CHARACTERISTICS , REMOTELY PILOTED VEHICLES


Subject Categories : Aerodynamics


Distribution Statement : APPROVED FOR PUBLIC RELEASE