- A design method for aircraft basic shapes with fully attached shock waves using known axisymmetric flow fields
Technical Report
CID:
Authors:
Publication Date:
- 01 March 1966
Publisher:
- Royal Aircraft Establishment
Place of Publication:
Class:
- RAE Report Collection
Series:
Series Number:
- 66069
Collation:
- 24 p.
Notes:
- (SER) Report also released in the series: Aircraft Research Committee Report ARC 28292
Publication Date Information:
- Mar 1966