Departure analysis of a twin-finned, high performance combat aircraft

21st Atmospheric Flight Mechanics Conference

Volumn , Issue , 1996, Pages 80-87

  Patel, Y ^a   Smith, P R ^a  

^a DEFENCE SCIENCE AND TECHNOLOGY LABORATORY   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; BIFURCATION (MATHEMATICS); FLIGHT ENVELOPES; ROOT LOCI; VEHICLE PERFORMANCE;

ANGLES OF ATTACK; BIFURCATION ANALYSIS; CLOSED LOOPS; COMBAT AIRCRAFT; CONTROL LAW DESIGN; NON LINEAR; OPEN-LOOP;

FIGHTER AIRCRAFT;

EID: 84983197016     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-3369     Document Type: Conference Paper

References (8)

1. C S Buttrill, P D Arbuckle, 'Simulation model of a twin-tail, high petformance airplane,' NASA Tech memo 107601, Langley Research Centre, Hampton, VA, 1992.
2. M Goman, A Khramtsovsky, 'Review of traditonal approaches in departure prediction,' Technical report TsAGI, Zhukovsky, Russia. October 1994.
3. G. J. Hancock, 'An introduction to the flight dynamics of rigid aeroplanes', Ellis Horwood, 1995.
4. J Kalviste, 'Aircraft stability characterstics at high angles of attack,' AGARD-CP-235, Paper 29, September 1978.
5. R Weissman, 'Preliminary criteria for predicting departure characteristics/spin susceptibility of fighter type aircraft,' Journal of Aircraft, Vol 10, No 4, 1973.
6. Y Patel, 'Departure prediction analysis of a high performance combat aircraft: Part II, DRA report DR A/AS/FDS/CR96199/1, May 1996.
7. M Goman, A Khramtsovsky, 'KRIT scientific package. User guide V2. 43,' Technical report TsAGI, Zhukovsky, Russia, 1993.
8. Etkin, B 'Dynamics of flight,' Wiley & Sons, 1959.