Actions for Wind-tunnel Tests of the 0.15-scale Powered Model of the Fleetwings XBTK-1 Airplane : Longitudinal Stability and Control

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Wind-tunnel Tests of the 0.15-scale Powered Model of the Fleetwings XBTK-1 Airplane : Longitudinal Stability and Control

Author
Weil, Joseph
Published
May 1945.
Physical Description
1 electronic document
Additional Creators
Boykin, Rebecca I.
Online Version

Availability

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
An investigation was made of the static longitudinal stability, and control and stall characteristics of XBTK-1 dive bomber. Results indicate that the longitudinal stability will probably be satisfactory for all contemplated flight conditions at the rear-most CG location with elevator both fixed and free. Power effects were small. Sufficient elevator control will be available to trim in any flight condition above the ground. Increasing the slotted flap deflection above 30 degrees only slightly increased the max. lift coefficient.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19930093674.
Accession ID: 93R22964.
NACA-WR-L-785.
NACA-MR-L5D27a.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15426687