Drag of closed cockpit and transport type windshields was determined from tests made at speeds corresponding to Mach number range of approximately 0.25 to 0.58 in NACA 8-ft high speed wind tunnel.
Investigation of drag of windshields in 8-foot high-speed wind tunnel
Nat Advisory Committee Aeronautics -- Report
1942
13 pages
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Wind tunnel tests of fuselages and windshields
NTRS | 1925
|Wind tunnel tests of fuselages and windshields
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Engineering Index Backfile | 1925
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