Identificatie
referentie code
BACH/B/1/11
Titel
'Ducted Cooling Tests Comparing the Normal Ring-Gill Exit with a Flap-Exit beneath the Wing'. Division of Aeronautics, Report No A10 by G K Batchelor
Datum(s)
- May 1942 (Vervaardig)
Beschrijvingsniveau
Stuk
Omvang en medium
1 doc