NASA Technical Note

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Flight Tests of a Twin-duct Induction System for a Mach Number Range of 0.78 to 2.07

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Growing Faith

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ÒFaith development cannot be divided into components. Rather it can be likened to the growth of a plant: seed, root, stem, leaf, bud, bloom. Each step happens

Structural Dynamic Model Obtained from Flight Use with Piloted Simulation and Handling Qualities Analysis

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Stability and Control Estimation Flight Test Results for the SR-71 Aircraft With Externally Mounted Experiments

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A maximum-likelihood output-error parameter estimation technique is used to obtain stability and control derivatives for the NASA Dryden Flight Research Center