Aerademetadata only
A theoretical and experimental investigation of the flow in a duct of varying cross-section, with particular application to the design of ducts for free flight ground-launched model tests
aerospace, aeronautics, engineering, aviation
This document is indexed with metadata only — full text is not available in the archive for this record.
Open the official source ↗
Related documents
Record · ID 491412
Conceptio Open Knowledge Archive — every document is proof-bundled with source, license, and retrieval metadata.