Wakefield, Roy M.
牋牋牋 NASA TM [X-92] : EFFECTS OF WING-CRANK, LEADING-EDGE EXTENSIONS AND HORIZONTAL-TALL HEIGHT ON THE LONGITUDINAL STABILITY OF SWEPT-WING MODELS AT MACH NUMBERS FROM 0.6 TO 1.4 / Roy M. Wakefield .- Nasa, Washington, D.C., 1959 .- 116 . .- ( NASA Technical Memorandum.
NASA Technical Memorandum X-71;72;75;83;85;86;89;92;100
Bounded Volumes Accession No. 102471; Contents: TR9389-96
Subject Headings:
Aerodynamics;
Copy Details:
Acc. No.: TR9395, Full Call No.: NASA TM X-92 -, Item type: Technical Report , Location: General Stacks,
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