Conceptio › Archive › Aerade

Aerademetadata only

Observations of the interaction between the shock waves and boundary layers at the trailing edges of aerofoils in supersonic flow

D. W. Holder et al.

Aerade · Other

Open Source ↗

aeronautics aerospace aviation engineering

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

Some details of the quintic profile for use in the polhausen-type of boundary-layer calculation#491743
A shock-expansion theory applicable to wings with attached shock waves#491744
Complex variable applications to certain coupled systems#491745
A technique for improving the predictions of linearised theory on the drag of straight-edged wings#491746
The influence of a model on plenum chamber indication of mach number in a slotted wall wind tunnel#491747

Record · ID 491405
Conceptio Open Knowledge Archive — every document is proof-bundled with source, license, and retrieval metadata.