Accession Number:

AD0005538

Title:

EFFECT OF FUEL INJECTORS AND LINER DESIGN ON PERFORMANCE OF AN ANNULAR TURBOJET COMBUSTOR WITH VAPOR FUEL

Descriptive Note:

Research memo.

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION CLEVELAND OH GLENN RESEARCH CENTER

Personal Author(s):

Report Date:

1953-04-06

Pagination or Media Count:

51.0

Abstract:

Subject Categories:

  • Pumps, Filters, Pipes, Tubing, Fittings and Valves
  • Combustion and Ignition

Distribution Statement:

APPROVED FOR PUBLIC RELEASE