Optimal supersonic intake design for air collection engines (ACE)

Citation
M. Valorani et al., Optimal supersonic intake design for air collection engines (ACE), ACT ASTRONA, 45(12), 1999, pp. 729-745
Citations number
21
Categorie Soggetti
Aereospace Engineering
Journal title
ACTA ASTRONAUTICA
ISSN journal
00945765 → ACNP
Volume
45
Issue
12
Year of publication
1999
Pages
729 - 745
Database
ISI
SICI code
0094-5765(199912)45:12<729:OSIDFA>2.0.ZU;2-B
Abstract
The success of Air Collection Engines (ACE) depends on the efficient integr ation of the many sub-systems involved. This article describes the tools de veloped to design a supersonic air intake of the mixed external/internal co mpression type that will feed the engine or the air liquefaction plant or b oth, during the different phases of the mission. One design procedure aims at finding the shape of minimum total pressure losses. An alternative strat egy aims at designing intakes which attain prescribed Mach number and flow deviation at the throat. Two design points are selected and their off-desig n behavior is predicted by space- and time-marching CFD models. The CFD ana lyses eventually provide the performance charts of the air intakes. (C) 200 0 Elsevier Science Ltd. All rights reserved.