Inlet DuctEngine Airflow Match and Compatibility for Supersonic Aircraft LJED, General Electric Company

Format:

Conference/Event

Author/Creator:

Alford, J. S., author.

Conference Name:

National Aerospace Engineering & Manufacturing Meeting

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1962

Summary:

A record of excellent compatibility with induction systems of all installations has been established by the J79 engine in six air weapons operating at Mach 2 and above. The paper discusses the aspects of steady state matching, dynamic matching, inflow distortion, and compressor design. Studies show that the engine must be evaluated as a component of the propulsion system, and that dynamic matching is at least as important as steady state matching for air breathing engines at Mach 3 and above

Notes:

Vendor supplied data

Publisher Number:

620300

Access Restriction:

Restricted for use by site license