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3rd Aerodynamic Deceleration Systems Conference, 1970
Abstract : The steady state flight performance of the Parafoil is computed by using aerodynamic coefficient data obtained from wind tunnel tests of both small scale models and full scale aspect ratio 2.0 units. The actual free flight performance of the Parafoil is obtained from both manned ascending flights and manned jumps from aircraft.
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Abstract : The steady state flight performance of the Parafoil is computed by using aerodynamic coefficient data obtained from wind tunnel tests of both small scale models and full scale aspect ratio 2.0 units. The actual free flight performance of the Parafoil is obtained from both manned ascending flights and manned jumps from aircraft.
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Data-enhanced dynamic flight simulations for flight performance analysis
Aerospace Science and Technology, 2022Dajung Kim, Arjit Seth, Rhea P Liem
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Thermal flight performance reveals impact of warming on bumblebee foraging potential
Functional Ecology, 2021Daniel Kenna +2 more
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A Method of Applying Flight Data to Evaluate Landing Operation Performance
Ergonomics, 2019Lei Wang, Jingyi Zhang
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