NASA / TN D-1959 -
Goldberg,Theodore J
EFFECTS OF ROUNDING CORNERS AND LEADING EDGES ON THE WINDWARD-SURFACE PRESSURE OF A DELTA WING SWEPT 65(DG) AT A MACH NUMBER OF 5.96 AT ANGLES OF ATTACK FROM 65(DG) TO 115(DG)AND ANGLES OF ROLL FROM.. / .- Nasa, Washington, D.C., 1963 .- 34 .
Bound With Nasa Tn D-1951-1960
Author Added Entry:
Blanchard,Doris K;
Copy Details:
Acc. No.: TR8715, Full Call No.: NASA TN D-1959 -, Item type: Technical Report , Location: General Stacks,
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Goldberg,Theodore J
EFFECTS OF ROUNDING CORNERS AND LEADING EDGES ON THE WINDWARD-SURFACE PRESSURE OF A DELTA WING SWEPT 65(DG) AT A MACH NUMBER OF 5.96 AT ANGLES OF ATTACK FROM 65(DG) TO 115(DG)AND ANGLES OF ROLL FROM.. / .- Nasa, Washington, D.C., 1963 .- 34 .
Bound With Nasa Tn D-1951-1960
Author Added Entry:
Blanchard,Doris K;
Copy Details:
Acc. No.: TR8715, Full Call No.: NASA TN D-1959 -, Item type: Technical Report , Location: General Stacks,
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