Landing Procedure in Model Ditching Tests of Bf 109
- Sottorf, W.
- December 1949.
- Physical Description:
- 1 electronic document
- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
- The purpose of the model tests is to clarify the motions in the alighting on water of a land plane. After discussion of the model laws, the test method and test procedure are described. The deceleration-time-diagrams of the landing of a model of the Bf 109 show a high deceleration peek of greater than 20g which can be lowered to 4 to 6g by radiator cowling and brake skid.
- NASA Technical Reports Server (NTRS) Collection.
- Document ID: 20050019585., NACA-TM-1247., and Wasserlandung Bf 109. Institut fuer Seeflugwesen er Deutschen Versuchaanstalt fuer Luftfahrt, E. V..
- No Copyright.
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