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Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform
U.S. Government
Paperback. Books LLC, Reference Series 2011-10-02.
ISBN 9781234336790
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Förlagets beskrivning
Original publisher: Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990. OCLC Number: (OCoLC)24899798 Subject: Drone aircraft -- Testing. Excerpt: ... S = 21.24 ft 2 b = 8.167t Cre f = 4.458 ft ( theoretical root chord ) Aileron and elevator chord increased 100 % i.::.:.:, :.:.:.:.:, :.::.::, :.:.:.:.:, :.:, :.:.:..:.:.:.:.:.:.:, :.:, _::::;; q.;; _, _. '. '. '. '. ". '. '. '. '.:::::::::::::::::::::: iiililiilili iii ! iiiiii L__ J_ 20 98 Notch. 625 deep x. 188 wide 42.5 ° ncreased vertical tail area J Recessed Increased tail moment arm Increased rudder area... _..: _.. > __: _: _ iiiliiii i_ wingtip fin @........... i.i.. i.. !..:.. i.i.i_.:. i:l !, i.i_iiii.V_1it7 Cross Wingtip fins added section ( a ) Overview. Figure 4. Three-view sketch of modified Exdrone RPV configuration. Dimensions are in inches unless otherwise specified. 11
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Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform
Bokrecensioner » Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform
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