Effects of airframe integrated configration on scramjet inlet performance

Daisuke Akihisa, Goro Masuya, Takeshi Kanda, Kouichiro Tani, Kenji Kudo

Research output: Contribution to conferencePaperpeer-review

1 Citation (Scopus)

Abstract

In order to examine the effects of the configuration of airframe integration on the scramjet inlet performance, preliminary calculations of the engine performance and wind tunnel tests were carried out for several types of the integrated inlet models. It was desirable to have an inlet inhaling the air compressed by the shock wave from the nose of the airframe, as well as to have the engine being integrated on the airframe paralleled to the airframe axis. In the experiment, the aerodynamic performances of the inlets were compared in terms of the total pressure efficiency and the mass capture ratio measured at the isolator. The experimental parameters were location of integration, type of compression, and strength of forebody compression. In the case that the inlet was attached on the ramp surface, and then turned parallel to the airframe axis, inlet (and the overall engine) showed good performances. This configuration could inhale the precompressed air effectively while reducing the cowl drag.

Original languageEnglish
Publication statusPublished - 2000
Event38th Aerospace Sciences Meeting and Exhibit 2000 - Reno, NV, United States
Duration: 2000 Jan 102000 Jan 13

Other

Other38th Aerospace Sciences Meeting and Exhibit 2000
CountryUnited States
CityReno, NV
Period00/1/1000/1/13

ASJC Scopus subject areas

  • Space and Planetary Science
  • Aerospace Engineering

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