Grumman X-29

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Grumman X-29
Grumman X-29 v letu
Vloga Eksperimentalno letalo
Izvor ZDA
Proizvajalec/-ci Grumman
Krstni polet 14. december 1984
Status Upokojen
Glavni uporabnik DARPA
Število izdelanih 2

Grumman X-29 je bilo ameriško eksperimentalno letalo namenjenu raziskovanju kril z negativnim naklonom, kanardov in drugih tehnologij. Letalo je bilo aerodinamično nestabilno zato je uporabljalo sistem fly-by-wire. Pri konstrukciji so uporabljali tudi kompozitne materiale. Prvič je poletel leta 1984, zgradili so dva prototipa ki so jih testirali naslednjih deset let.

X-29 kokpit

Specifikacije(X-29)[uredi | uredi kodo]

Grumman X-29 outline.svg

Podatki iz NASA X-Planes

Splošne karakteristike

Zmogljivost

  • Maks. hitrost: Mach 1.8 (1100 mph, 1770 km/h na 33000 čevljih (10000 m))
  • Doseg: 350 milj (560 km)
  • Višina leta: 55000 ft (16800 m)

Glej tudi[uredi | uredi kodo]

Reference[uredi | uredi kodo]

Bibliografija[uredi | uredi kodo]

  • Butts, S. L.; Hoover, A. D. (May 1989). "Flying Qualities Evaluation of the X-29A Research Aircraft". U.S. Air Force Flight Test Center. AFFTC-TR-89-08. 
  • Donald, David, ur. (1997). "Grumman X-29A". The Complete Encyclopedia of World Aircraft. New York: Barnes & Noble. ISBN 0-7607-0592-5. 
  • Green, William (1970). Warplanes of the Third Reich. New York: Doubleday. ISBN 0-385-05782-2. 
  • Jenkins, Dennis R.; Landis, Tony; Miller, Jay (June 2003). American X-Vehicles: An Inventory—X-1 to X-50 (PDF). Monographs in Aerospace History No. 31. NASA. OCLC 68623213. SP-2003-4531. 
  • Pamadi, Bandu N. (2004). Performance, Stability, Dynamics, and Control of Airplanes (2nd izd.). American Institute of Aeronautics and Astronautics. ISBN 978-1-56347-583-2. doi:10.2514/4.862274. 
  • Putnam, Terrill W. (January 1984). X-29 Flight-Research Program (PDF). AIAA 2nd Flight Test Conference. Las Vegas, Nevada. 16-18 November 1983. NASA. TM-86025. 
  • Roskam, Jan (1985). Airplane Design, Part II: Preliminary Configuration Design and Integration of the Propulsion System. Ottawa, Kansas: Roskam Aviation and Engineering Corporation. ISBN 978-1-88488-543-3. 
  • Thruelsen, Richard (1976). The Grumman Story. New York: Praeger Publishers. ISBN 0-275-54260-2. 
  • Treadwell, Terry (1990). Ironworks: Grumman's Fighting Aeroplanes. Shrewsbury, UK: Airlife Publishers. ISBN 1-85310-070-6. 
  • Warwick, Graham (16 June 1984). "Forward-sweep Technology". Flight International: 1563–1568. 
  • Webster, Frederick R.; Purifoy, Dana (July 1991). X-29 High Angle-of-Attack Flying Qualities. U.S. Air Force Flight Test Center. AFFTC-TR-91-15. 
  • Winchester, Jim (2005). "Grumman X-29". X-Planes and Prototypes. London: Amber Books. ISBN 1-904687-40-7. 

Zunannje povezave[uredi | uredi kodo]