Accession Number : ADA111784

Title :   Current Status of Inlet Flow Prediction Methods,

Corporate Author : BOEING MILITARY AIRPLANE CO SEATTLE WA

Personal Author(s) : Paynter,Gerald C

PDF Url : ADA111784

Report Date : 14 May 1981

Pagination or Media Count : 36

Abstract : The increasing availability of large computers, advances in numerical fluid mechanics, and the rapidly escalating cost of wind tunnel testing are responsible for a trend toward the use of parametric analysis rather than parametric testing to support the design of inlet systems. With an emphasis on the transonic and supersonic speed regimes, current approaches to inlet flow analysis are discussed in the context of the inlet design process. Results from typical procedures now under development for supersonic inlet flows are presented along with a discussion of the advantages and disadvantages of each for design. The requirements for experimental validation of a procedure and analysis problem areas are reviewed. Recent developments which may lead to an improved inlet flow analysis capability are discussed. (Author)

Descriptors :   *Jet engine inlets, Computer aided design, Supersonic flow, Transonic flow, Subsonic flow, Parametric analysis, Three dimensional flow, Two dimensional flow, Mathematical prediction, Inlets, Flow fields

Subject Categories : Fluid Mechanics
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE