A remarkable aerodynamic performance of triangle cross section configuration for fully RLV

Shigeru Aso, Yasuhiro Tani, Takuro Ishida

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

An experimental study for improving the aerodynamic characteristics of wing-body configuration RLVs has been conducted. The fuselage cross-sectional configurations are isosceles right triangle and square with rounded corners. The models have single-delta wings modified NACA 0010 with 45 deg sweepback angle. The experiments were conducted in a transonic and supersonic wind tunnel at ISAS(Institute of Space and Astronautical Science), JAXA(Japan Aerospace Exploration Agency). Test conditions were as follows: Free stream mach numbers were from 0.3 to 4.0. Angles of attack were changed from -15 deg to 40 deg, but by the limitation of balance load, some cases were tested with up to 15 deg. The experimental results have shown that the model with isosceles right triangle cross-sectional configuration had good aerodynamic characteristics in the region from subsonic to supersonic, i.e. triangle model has better lift coefficient and lift-to-drag ratio than square model.

Original languageEnglish
Title of host publication61st International Astronautical Congress 2010, IAC 2010
Pages6375-6379
Number of pages5
Publication statusPublished - Dec 1 2010
Event61st International Astronautical Congress 2010, IAC 2010 - Prague, Czech Republic
Duration: Sep 27 2010Oct 1 2010

Publication series

Name61st International Astronautical Congress 2010, IAC 2010
Volume8

Other

Other61st International Astronautical Congress 2010, IAC 2010
CountryCzech Republic
CityPrague
Period9/27/1010/1/10

Fingerprint

aerodynamics
triangles
Aerodynamics
aerodynamic characteristics
cross sections
configurations
sweepback
body-wing configurations
transonic wind tunnels
supersonic wind tunnels
delta wings
lift coefficients
fuselages
Fuselages
aerospace sciences
angle of attack
free flow
Angle of attack
Mach number
drag

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Astronomy and Astrophysics

Cite this

Aso, S., Tani, Y., & Ishida, T. (2010). A remarkable aerodynamic performance of triangle cross section configuration for fully RLV. In 61st International Astronautical Congress 2010, IAC 2010 (pp. 6375-6379). (61st International Astronautical Congress 2010, IAC 2010; Vol. 8).

A remarkable aerodynamic performance of triangle cross section configuration for fully RLV. / Aso, Shigeru; Tani, Yasuhiro; Ishida, Takuro.

61st International Astronautical Congress 2010, IAC 2010. 2010. p. 6375-6379 (61st International Astronautical Congress 2010, IAC 2010; Vol. 8).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Aso, S, Tani, Y & Ishida, T 2010, A remarkable aerodynamic performance of triangle cross section configuration for fully RLV. in 61st International Astronautical Congress 2010, IAC 2010. 61st International Astronautical Congress 2010, IAC 2010, vol. 8, pp. 6375-6379, 61st International Astronautical Congress 2010, IAC 2010, Prague, Czech Republic, 9/27/10.
Aso S, Tani Y, Ishida T. A remarkable aerodynamic performance of triangle cross section configuration for fully RLV. In 61st International Astronautical Congress 2010, IAC 2010. 2010. p. 6375-6379. (61st International Astronautical Congress 2010, IAC 2010).
Aso, Shigeru ; Tani, Yasuhiro ; Ishida, Takuro. / A remarkable aerodynamic performance of triangle cross section configuration for fully RLV. 61st International Astronautical Congress 2010, IAC 2010. 2010. pp. 6375-6379 (61st International Astronautical Congress 2010, IAC 2010).
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