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- W2099708071 abstract "We summarize the work accomplished over the last several years on wake-survey analysis method developments at Boeing. Betz and Maskell's lift-and-drag equations are extended to cover compressible flows. The small perturbation method is employed to expand the general lift-and-drag equations in the momentum integral forms, assuming downstream states that differ only slightly from the state of approach. Introducing new, simpler, and cleaner expansion procedures, it is proven that both the lift and drag of an airplane model can be predicted accurately by simply measuring flow variables inside of the model wake region. This result enables the practical application of quantitative wake surveys for accurate lift-and-drag predictions of airplane models. To demonstrate the current lift-and-drag prediction capabilities, some wake-survey analysis results from previously published data are recalculated. Because wake surveys are not needed outside of the model wake region, one complete wake survey analysis for a nonpowered engine case, including data acquisitions and reductions, can now be finished in approximately 10-15 min" @default.
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- W2099708071 date "2002-11-01" @default.
- W2099708071 modified "2023-09-26" @default.
- W2099708071 title "Extension of Wake-Survey Analysis Method to Cover Compressible Flows" @default.
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- W2099708071 doi "https://doi.org/10.2514/2.3048" @default.
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