Estimating aerodynamic characteristics of the alflex vehicle using flight test data

22nd Atmospheric Flight Mechanics Conference

Volumn , Issue , 1997, Pages 33-41

  Yanagihara, Masaaki ^a   Shigemi, Masashi ^a   Suito, Takanobu ^a  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT LANDING; DELTA WING AIRCRAFT; LANDING; VEHICLES; VERTICAL STABILIZERS; WIND TUNNELS;

AERODYNAMIC CHARACTERISTICS; AUTOMATIC LANDING; DELTA WINGS; FLIGHT EXPERIMENTS; FLIGHT TEST DATA; SURFACE EXCITATIONS; UMBILICAL CABLES; WIND TUNNEL TESTS;

CONTROL SURFACES;

EID: 84983179934     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. Nagayasu, M. et al. Automatic Landing Flight Experiment (ALFLEX) using a HOPE Scaled Model, Research Progress of National Aerospace Laboratory 1996
2. Tsukamoto, T. et al. ALFLEX Five Degrees of Freedom Hanging Flight Test, AIAA Atmospheric Flight Mechanics Conference, AIAA-97-3484 (1997)
3. Nagayasu, M. et al. On the Interactive Computer Program IPIS for Aircraft Parameter Identification, Technical Report of National Aerospace Laboratory TR-1000 (1988) (In Japanese)
4. Yanagihara, M. et al. Suspending Wind-Tunnel Test for ALFLEX Vehicle, Technical Report of National Aerospace Laboratory TR-1306 (1996) (In Japanese)