Aerodynamic performance enhancement by lateral blowing for reusable launch vehicles

Kenji Tadakuma, Shigeru Aso, Yasuhiro Tani

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

Abstract

An experimental study on the improvement of aerodynamic characteristics of RLVs (Reusable Launch Vehicles) due to lateral blowing has been conducted. A square and a triangular cross sections of fuselage have been considered in order to investigate effects of shape of cross section of fuselage on aerodynamic characteristics during lateral blowing. And four different planform wings have been considered to evaluate effects on planform of wing during lateral blowing. Results show that lateral blowing increases lift of the models over a wide range of angle of attack. Especially a significant increase in lift is achieved in the case of a "square" model at high angle of attack. Increase of lift due to lateral blowing is obtained in all wing types over a wide range of angle of attack. The resulting lift of the model with small sweepback angle and a rectangular wing is lager than that of the other wings in high angle of attack region. As a result of calculation of landing process, lateral blowing makes possible a shorter landing distance or a smaller landing velocity of a RLV.

Original languageEnglish
Title of host publicationAIAA 57th International Astronautical Congress, IAC 2006
Pages7663-7677
Number of pages15
Publication statusPublished - Dec 1 2006
EventAIAA 57th International Astronautical Congress, IAC 2006 - Valencia, Spain
Duration: Oct 2 2006Oct 6 2006

Publication series

NameAIAA 57th International Astronautical Congress, IAC 2006
Volume11

Other

OtherAIAA 57th International Astronautical Congress, IAC 2006
CountrySpain
CityValencia
Period10/2/0610/6/06

Fingerprint

reusable launch vehicles
blowing
Launch vehicles
Blow molding
aerodynamics
Aerodynamics
angle of attack
Angle of attack
augmentation
landing
Landing
wings
aerodynamic characteristics
Planforms
fuselages
Fuselages
cross section
sweepback
wing planforms
rectangular wings

All Science Journal Classification (ASJC) codes

  • Space and Planetary Science
  • Aerospace Engineering

Cite this

Tadakuma, K., Aso, S., & Tani, Y. (2006). Aerodynamic performance enhancement by lateral blowing for reusable launch vehicles. In AIAA 57th International Astronautical Congress, IAC 2006 (pp. 7663-7677). (AIAA 57th International Astronautical Congress, IAC 2006; Vol. 11).

Aerodynamic performance enhancement by lateral blowing for reusable launch vehicles. / Tadakuma, Kenji; Aso, Shigeru; Tani, Yasuhiro.

AIAA 57th International Astronautical Congress, IAC 2006. 2006. p. 7663-7677 (AIAA 57th International Astronautical Congress, IAC 2006; Vol. 11).

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

Tadakuma, K, Aso, S & Tani, Y 2006, Aerodynamic performance enhancement by lateral blowing for reusable launch vehicles. in AIAA 57th International Astronautical Congress, IAC 2006. AIAA 57th International Astronautical Congress, IAC 2006, vol. 11, pp. 7663-7677, AIAA 57th International Astronautical Congress, IAC 2006, Valencia, Spain, 10/2/06.
Tadakuma K, Aso S, Tani Y. Aerodynamic performance enhancement by lateral blowing for reusable launch vehicles. In AIAA 57th International Astronautical Congress, IAC 2006. 2006. p. 7663-7677. (AIAA 57th International Astronautical Congress, IAC 2006).
Tadakuma, Kenji ; Aso, Shigeru ; Tani, Yasuhiro. / Aerodynamic performance enhancement by lateral blowing for reusable launch vehicles. AIAA 57th International Astronautical Congress, IAC 2006. 2006. pp. 7663-7677 (AIAA 57th International Astronautical Congress, IAC 2006).
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