Accession Number : AD0218806

Title :   APPLICATION OF DIRECT ENGINE THRUST MEASUREMENTS IN SUPERSONIC AND HYPERSONIC FLIGHT REGIMES

Corporate Author : ADVISORY GROUP FOR AERONAUTICAL RESEARCH AND DEVELOPMENT PARIS (FRANCE)

Personal Author(s) : DETTWYLER, H.R.

Report Date : APR 1958

Pagination or Media Count : 19

Descriptors :   *CANTILEVER BEAMS, *RAMJET ENGINES, MEASUREMENT, SUPERSONIC FLOW, THRUST.

Distribution Statement : APPROVED FOR PUBLIC RELEASE