Thrust vectoring and tailless aircraft design - Review and outlook

21st Atmospheric Flight Mechanics Conference

Volumn , Issue , 1996, Pages 420-430

  Friehmelt, Holger ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC DRAG; AERODYNAMICS; AIRCRAFT; FLIGHT SIMULATORS; RADAR CROSS SECTION;

AERODYNAMIC CHARACTERISTICS; ANALYTICAL DESCRIPTION; IN-FLIGHT SIMULATION; KEY TECHNOLOGIES; PROOF OF CONCEPT; TAILLESS AIRCRAFT; TECHNICAL REALIZATION; THRUST VECTORING;

VERTICAL STABILIZERS;

EID: 84983146584     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-3412     Document Type: Conference Paper

References (24)

1. Skow, A. M.: Agility as a Contribution to Design Balance. AIAA Paper 90-1305, AIAA/SFTE/DGLR/SETP 5 Biannual Flight Test Conference, Ontario, CA, May 22-24, 1990.
2. Dornheim, M. A. and Hughes, D.: America's Short Range Missile Handicap, Parti. Aviation Week & Space Technology, Oct 16, 1995, pp. 36-49.
3. Bartoldus, K. H.: Heimet Mounted Visual Audio Display (HMVAD) Symboiogy Evaluation during X-31 Tactical Utility Flight Test Deutsche Aerospace, Dasa/LME11/X-31/TN/85, Ottobrunn, May 1994.
4. Gal Or, B.: Vectored Propulsion, Supermaneuverability and Robot Aircraft Springer-Verlag, Berlin, Heidelberg, New York, ISBN 3-540-97161-0, 1990.
5. th High Alpha Conference, NASA CP-10143, Edwards, CA, Jul 12-14. 1994.
6. Ross, H.: X-31 Enhancement of Aerodynamics for Maneuvering beyond Stall. AGARD CP-497, 1991, pp. 2. 1-2. 12.
7. lrodov, R. D. and Petrov, A. V.: Aerodynamic Design of Super Maneuverable Aircraft. AGARD Flight Mechanics Panel Symposium, Annapolis, MD, Oct 18-21, 1993, AGARD CP-548, pp. 12. 1-12, 6.
8. Chambers, J. R. and Grafton, S. B.: Aerodynamic Characteristics of Airplanes at High Angies of Attack. Langley, NASA TM-74097, 1977.
9. Barham, R. W.: Thrust Vector Aided Maneuvering of the YF-22 Advanced Tactical Fighter Prototype. AGARD Flight Mechanics Panel Symposium, Annapolis, MD, Oct 18-21, 1993, AGARD CP-548, pp. 5. 1-5. 14.
10. th Annual Symposium of the Society of Flight Test Engineers (SFTE) Open Sky,' Berlin, June 19-23, 1995.
11. Friehmelt, H.; Plaetschke, E.; Rohlf, D.; and Weib, S.: EFM/X-31A; DLR-USA-Unterstiitzung für den Zeitraum 01. 01. 199504. 09. 1995. Abschlu-bericht für BMVg I BWB-Auftrag E/L41L/Q0255/N5122, DLR-IB 111-95/35, October 1995.
12. Baumgarten, G.; Buchholz, J. J.; and Heine, W.: A New Reconfiguration Concept for Flight Control Systems. AIAA Guidance, Navigation, and Control Conference, Paper AIAA 95-3176-CP, Baltimore, MD, Aug 6-10, 1995.
13. Francis, M. S.: X-31: An International Success Story. Aerospace America, Feb '95, pp. 22-27, 32.
14. th ICAS Congress, Sorrento, Italy, Sept. 8-13, 1996.
15. Banks, D. W:; Quinto, P. F.; and Paulson, J. W. Jr.: Thrust-Induced Effects on Low-Speed Aerodynamics of Fighter Aircraft AIAA Paper 81-2612, AIAA/NASA Ames V/STOL Conference, Palo Alto, CA, Dec 7-9, 1981.
16. Bowers, A. H. et al.: Multiaxis Thrust Vectoring Using Axisymmetric Nozzles and Pastexit Vanes on an F/A-18 Configuration Vehicle. NASA Dryden, NASA TM-101741, 1991.
17. Lang, K.-H. and Richter, H.: X-31 Mehr als nur ein Experiment Soldat und Technik, June 1995, pp. 347-353.
18. Huber, P.: Control Law Design for Tailless Confígurations and InFlight Simulation Using the X-31 Aircraft. AIAA Guidance, Navigation, and Control Conference, Paper AIAA 95-3199-CP, Baltimore, MD, 6.-10. Aug. 1995, pp. 247-257.
19. Lichte, R.: Die Radar-Reichweitenformei Soldat und Technik, Vol. 38 (1995), No. 10, p. 632.
20. Whitford, R.: Fundaments of Fighter Design Part 1-Requirements. Air International, Vol. 50 (1996), No, 1, pp. 37-43.
21. Raymer, D.: Aircraft Design: A Conceptual Approach. AIAA Education Series. ISBN 0-930403-51-7, 1989.
22. Jategaonkar, R. V., Thielecke, F.: Evaluation of Parameter Estimation Methods for Unstable Aircraft. Journal of Aircraft, Vol. 31, No. 3, May-June 1994, pp. 510-519.
23. Galleithner, H.: X-31A Dynamic Stability Parameters Summary. DLR-IB 111-92/29, 1992.
24. th Annual Symposium of the Society of Flight Test Engineers (SFTE) 'Open Sky,' Berlin, June 19-23, 1995, pp. 2. 27-2. 38.