ASD Advanced Program Research Inlet Data Analysis Report for 1/5.2-Scale Model Inlet Tests.

摘要

The analysis of wind-tunnel data from tests of a 1/5.2-scale inlet research model covered was conducted. Inlet design and engine/inlet compatibility criteria are based on the F101-GE-100 engine characteristics and requirements. Detailed inlet flow-field analyses are discussed. Inlet pressure recovery, distortion, and compatibility parameters are presented for a basic configuration from Mach 0.55 to Mach 2.0. Data for an alternate configuration are presented for Mach 0.55 to 1.5. A limited amount of data are also presented for other configurations that were tested. (Author)