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

Abstract

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)

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1977
Accession Number
ADA040707

Entities

People

  • Charles C. Mann
  • Jack E. Garner

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Airframes
  • Analog Computers
  • Boundary Layer
  • Capillary Electrophoresis
  • Duct Bends
  • Flow Fields
  • Instrumentation
  • Leading Edges
  • Lepidoptera
  • Mach Number
  • Model Tests
  • Performance Engineering
  • Static Pressure
  • Steady State
  • Vortex Generators

Readers

  • Aerodynamics.
  • Systems Analysis and Design