Accession Number:

AD0238250

Title:

A FLIGHT TEST METHOD TO DETERMINE OPTIMUM RANGE DESCENT CONDITIONS IN A TURBOJET AIRCRAFT

Descriptive Note:

Corporate Author:

PRINCETON UNIV NJ JAMES FORRESTAL RESEARCH CENTER

Report Date:

1960-05-16

Pagination or Media Count:

1.0

Abstract:

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE