The X-31 - High performance at low cost

Author:

POWERS SIDNEY1,SCHELLENGER HARVEY1

Affiliation:

1. Rockwell International Corp., El Segundo, CA

Publisher

American Institute of Aeronautics and Astronautics

Cited by 7 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Assessment of Sting Effect on X-31 Aircraft Model Using CFD;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04

2. Application of Volterra Functions to X-31 Aircraft Model Motion;27th AIAA Applied Aerodynamics Conference;2009-06-14

3. The X-31: A Post-Stall Technology (PST) Fighter Close-In-Combat Results Assessment, And A Look At New CIC Performance Evaluation Metrics;AIAA Atmospheric Flight Mechanics Conference and Exhibit;2004-06-22

4. Flying Qualities, Unstable Flight, Avionics, Cockpit, Sensors;Aeronautical Research in Germany;2004

5. The X-31 experience - Aerodynamic impediments to post-stall agility;33rd Aerospace Sciences Meeting and Exhibit;1995-01-09

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