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- W2327967908 abstract "Tlic design prograin system PrADO-Hy (Preliminxy ift Design and Optimization Hypersonic) for the computer-aided conception:il design of hypeixonic aircr;lfts, developed hy the Institute of Aircraft Design :tiid Structure Mechanics, is introduced. The modu1:u prograin si~nul;ites in it’s kernel the design process with the intcr:icrions tihle optitnkition loop. The practical :ipplic:ition of the program system is dcinonstr;ued hy ii design study of two TSTO vehicles, :illowing ii cruise llight with the orhiter from Europe to the Equator which should transfer :I p:iyload of 3.7 t I D LEO. For tlic lower st:igc two concepts iue investigated: :I liltiiig hody conligur;ition ;urd ii w:iverider The ckiss 01 waveriders considered i n this paper have ir lift over c1r:ig ratio of ahout 7 (including lriction drag) ;it M;i = 4.5 ;ind provide sufficient volutnc for the intcgr;ition of tanks. p m pulsion group, ctc. Tlicy were designed using the oscuI:iling cone method. Tlic investigations show, that :I TSTO vehicle liming :I waverider a it’s first stage will have ii take-off weight of ahout 3” 1, 4 engines and a Grnwtli f:ictor of 90.3. whcras the lifting hody design will he 30% 1rc:ivicr. nccds 6 engines :ind h:is a Growth factor ( i t" @default.
- W2327967908 created "2016-06-24" @default.
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- W2327967908 date "1993-08-22" @default.
- W2327967908 modified "2023-09-25" @default.
- W2327967908 title "Investigations on the potential of hypersonic waveriders with the integrated aircraft design program PrADO-Hy" @default.
- W2327967908 doi "https://doi.org/10.2514/6.1993-5098" @default.
- W2327967908 hasPublicationYear "1993" @default.
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