Supersonic experimental airplane (NEXST) for next generation SST technology - Development and flight test plan for the unmanned scaled supersonic glider

40th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2002, Pages

  Sakata, Kimio ^a  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BOUNDARY LAYERS; COMPUTATIONAL FLUID DYNAMICS; INVERSE PROBLEMS; ROCKETS; SOFTWARE TESTING; TESTING; TRANSPORT AIRCRAFT;

AERODYNAMIC DESIGN TECHNOLOGY; CFD (COMPUTATIONAL FLUID DYNAMICS); INVERSE DESIGN METHODS; NATIONAL AEROSPACE LABORATORIES; SOLID ROCKET BOOSTERS; SUPERSONIC TRANSPORT; SURFACE STATIC PRESSURE; TECHNOLOGY DEVELOPMENT;

SUPERSONIC AIRCRAFT;

EID: 85088758520     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-527     Document Type: Conference Paper

References (3)

1. Sakata, Kimio., (3rd International Workshop on CFD for SST design), NAL-SP-49T, December 2000
2. Yoshida, K, Special Course at VKI, RTOEN4, 15-1,1998
3. T. Iwamiya et al, (in Japanese)", Jl. of Fluid