NASA / TN D-398
Llewellyn,Charles P
EFFECT OF REYNOLDS NUMBER ON THE LATERAL-STABILITY DERIVATIVES AT LOW SPEED OF SWEPTBACK- AND DELTA-WING-FUSELAGE COMBINATIONS OSCILLATING IN YAW
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.- Nasa, Washington, D.C., 1960
.- 45 .
Bound With Nasa Tn D-391-97,399-400
Author Added Entry:
Wolhart,Walter D;
Copy Details:
Acc. No.: TR15931, Full Call No.: NASA TN D-398, Item type: Technical Report , Location: General Stacks,
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