X-31 vector aircraft, low speed stability & control, comparisons of wind tunnel data & theory (focus on linear & panel codes)

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn , Issue , 2009, Pages

  Nangia, R K ^a  

^a Nangia Aero Research Associates   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; FLIGHT CONTROL SYSTEMS; FLIGHT DYNAMICS; POTENTIAL FLOW; STABILITY; WIND TUNNELS;

ASYMMETRIC EFFECTS; COMPLEX CONFIGURATION; LONGITUDINAL STABILITY; PREDICTION METHODS; STABILITY AND CONTROL; STABILITY DERIVATIVES; SURFACE SINGULARITY METHOD; X-31 VECTOR AIRCRAFT;

RESEARCH AIRCRAFT;

EID: 85067319720     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-3898     Document Type: Conference Paper

References (7)

1. Data Reports, DLR.
2. NANGIA, R.K. & PALMER, M.E., "Application of Subsonic First-Order Methods for Prediction of Inlet & Nozzle Aerodynamic Interactions with Airframe", Symposium on "Aerodynamic Engine/Airframe Integration for High Performance Aircraft & Missiles", Fort Worth, Texas, USA, AGARD CP-498, 1991.
3. NANGIA, R. K., "Low Speed Performance Optimisation of Advanced Supersonic Civil Transport with Different LE & TE Devices", EAC'94, Toulouse, France, October 1994.
4. NANGIA, R.K. & MILLER, A.S., "Vortex Flow Dilemmas & Control on Wing Planforms for High Speeds", Paper Presented at RTO - AVT Symposium, Loen, Norway, May 2001.
5. Report for AVT-161 Task Group.
6. NANGIA, R.K., "Semi-Empirical Prediction of the Vortex Formation on the VFE-2 Configuration (65 deg. Delta Wings with different Leading Edge shapes) ", Chapter 33, RTO-AVT-113 Report, Formal Publication 2008.
7. NANGIA, R.K., "Semi-Empirical Prediction of the Vortex Onset & Progression on 65 deg. Delta Wings (RTO-AVT-113, VFE-2 Facet) ", 46th AIAA Aerospace Sciences. Meeting, Reno, AIAA-2008-10384, January 2008.