ANALYSIS OF A.E.L. NOZZLE TESTS

Abstract

The data from cold flo tests of two jet flap nozzle is analyzed. These tests were conducted in an altitude chamber. Airflow, the Mach number in the inlet and at the slot, the nozzle thrust distribution, ischarge coefficient, and pressure loss coefficient are derived in the analysis. (Author)

Document Details

• Document Type: Technical Report
• Publication Date: Jun 09, 1961
• Accession Number: AD0260990

Tags

DTIC Thesaurus Topics

• Altitude
• Altitude Chambers
• Chambers
• Coefficients
• Jet Flaps
• Mach Number
• Pressure Distribution

Fields of Study

• Physics

Readers

• Aerospace Engineering
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