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A new method for numerical integration of airplane equations of motion c20031104 [2].pdf 296KB Mar 29 2010 08:59:58 AM

A system to vary the stability and control of a deflected-jet, fixed-wing vtol aircraft c20031104 [5].pdf 1274KB Mar 29 2010 08:59:58 AM

A Word of Appreciation c20031104 [1].pdf 124KB Mar 29 2010 08:59:58 AM

Erratum_ _Sample Estimates of B-66B Low-Level, Clear-Air Gust Field Parameters_ c20031104 [1].pdf 104KB Mar 29 2010 08:59:58 AM

Erratum_ _Some Opportunities for Progress in Aircraft Performance_ c20031104 [1].pdf 104KB Mar 29 2010 08:59:58 AM

Influence of fan and ducting characteristics on the stability of ground effect machines c20031104 [8].pdf 876KB Mar 29 2010 08:59:58 AM

Measurements of fluctuating air loads on a circular cylinder c20031104 [7].pdf 1087KB Mar 29 2010 08:59:58 AM

Pt6 turboprop for general aviation c20031104 [5].pdf 1100KB Mar 29 2010 08:59:58 AM

Some important design considerations on the xc- 142a triservice vstol c20031104 [4].pdf 438KB Mar 29 2010 08:59:58 AM

The neutral point in stability and control analysis c20031104 [6].pdf 695KB Mar 29 2010 08:59:58 AM

Thermal stress and instability of sandwich cylinders on rigid supports c20031104 [5].pdf 576KB Mar 29 2010 08:59:58 AM

Vectored thrust engines for single and multiengined aircraft c20031104 [7].pdf 1547KB Mar 29 2010 08:59:58 AM

X-22a design development c20031106 [7].pdf 2631KB Mar 29 2010 08:59:58 AM