Application of large-angle data for flight simulation

Modeling and Simulation Technologies Conference

Volumn , Issue , 2000, Pages

  Dickes, Edward G ^a   Ralston, John N ^a   Lawson, Kenneth P ^b  

^a Bihrle Applied Research Inc   (United States)

^b NAVAL AIR SYSTEMS COMMAND   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; MACHINERY; SUPERSONIC AIRCRAFT; WIND TUNNELS;

AERODYNAMIC SIMULATIONS; FLIGHT SIMULATION; LARGE ANGLE OF ATTACKS; LEADING EDGE FLAPS; SIMULATION MODEL; STATIC AND DYNAMIC TESTS; TRAILING EDGE FLAPS; WIND-TUNNEL DATA;

FLIGHT SIMULATORS;

EID: 85087192986     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-4584     Document Type: Conference Paper

References (3)

1. Dickes, E., Ralston, J. and Kloc, S., "F-18E Large-Angle Testing: Static and Dynamic Characteristics From Rotary Balance Wind Tunnel Test Data and Aeromodel Increments", BAR 99-05, June 1999.
2. Kay, J.,"F-18E/F FEB98AERO Model Rehost Static Check Case Verification Results", BAR 99-07M, July 1999.
3. Kalviste, Juri: Use of Rotary Balance And Forced Oscillation Test Data In A Six Degrees Of Freedom Simulation, AIAA Paper 82-1364, August 1982.