Accession Number : AD0091959


Title :   PERFORMANCE OF SUPERSONIC RAMP-TYPE SIDE INLET WITH COMBINATIONS OF FUSELAGE AND INLET THROAT BOUNDARY-LAYER REMOVAL


Descriptive Note : Research memo.


Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON DC


Personal Author(s) : CAMPBELL, ROBERT C


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/091959.pdf


Report Date : 25 Apr 1956


Pagination or Media Count : 25


Descriptors :   *FUSELAGES , *DUCT INLETS , *BOUNDARY LAYER CONTROL , SUPERSONIC FLOW


Subject Categories : Aircraft
      Pumps, Filters, Pipes, Tubing, Fittings & Vlvs


Distribution Statement : APPROVED FOR PUBLIC RELEASE