NASA NTRS · 19780016126
Inlet technology for powered-lift aircraft
Abstract
The concepts, analytical tools, and experimental data available for designing inlets for powered lift aircraft are discussed. It is shown that inlets can be designed to meet noise, distortion, and cruise drag requirements at the flight and engine operating conditions of a powered lift aircraft. The penalty in pressure recovery for achieving the required noise suppression was 0.3 percent.
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Luidens, R. W.. 1976-01-01. Inlet technology for powered-lift aircraft. https://ntrs.nasa.gov/citations/19780016126
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