NASA / MEMO 4-3-59L -
Margolis,Kenneth
FORMULAS PERTINENT TO THE CALCULATION OF FLOW-FIELD EFFECTS AT SUPERSONIC SPEEDS DUE TO WING THICKNESS / .- Nasa, Washington, D.C., 1959 .- 26 .
Bound With Nasa Memo 4-1-59l-4-19-59l
Author Added Entry:
Elliott,Miriam H;
Copy Details:
Acc. No.: TR7688, Full Call No.: NASA MEMO 4-3-59L -, Item type: Technical Report , Location: General Stacks,
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Margolis,Kenneth
FORMULAS PERTINENT TO THE CALCULATION OF FLOW-FIELD EFFECTS AT SUPERSONIC SPEEDS DUE TO WING THICKNESS / .- Nasa, Washington, D.C., 1959 .- 26 .
Bound With Nasa Memo 4-1-59l-4-19-59l
Author Added Entry:
Elliott,Miriam H;
Copy Details:
Acc. No.: TR7688, Full Call No.: NASA MEMO 4-3-59L -, Item type: Technical Report , Location: General Stacks,
------------------------- --------------------- ------ --------- ------- ------- --------- --------