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An Approximate Spin Design Criterion for Monoplanes

Free spinning wind-tunnel tests of a low-wing monoplane with systematic wings and tails 2: Mass distributed along the fuselage

Free-spinning wind-tunnel tests of a low-wing monoplane with systemic changes in wings and tails 1: Basic loading condition

Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails 3: mass distributed along the wings

Comparison of free-spinning wind-tunnel results with corresponding full-scale spin results

Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails IV: effect of center-of-gravity location

Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails V: effect of airplane relative density

Spin tests of a low-lying monoplane in flight and in the free-spinning wind tunnel

Elevator Stick Forces in Spins as Computed From Wind-Tunnel Measurements

Influence of Loading Condition on Piloting Technique for Spin Recovery for Pursuit Airplanes

Multiengine airplane spin characteristics as indicated by model tests in the free-spinning wind tunnel

Spinning of Large Airplanes


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