NASA / MEMO 1-22-59L
Boisseau,Peter C
LOW-SUBSONIC STATIC STABILITY AND DAMPING DERIVATIVES AT ANGLES OF ATTACK FROM 0 DEGREE TO 90 DEGREE FOR A MODEL WITH A LOW-ASPECT-RATIO UNSWEPT WING AND TWO DIFFERENT FUSELAGE FOREBODIES / .- Nasa, Washington, D.C., 1959 .- 25 .
Bound With Nasa Memo 1-15-59l-20,23-31 Lack No.1-18-59l-1-19-59l,1-21-59l,1-28-59l-1-29-59l
Copy Details:
Acc. No.: TR17736, Full Call No.: NASA MEMO 1-22-59L, Item type: Technical Report , Location: General Stacks,
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Boisseau,Peter C
LOW-SUBSONIC STATIC STABILITY AND DAMPING DERIVATIVES AT ANGLES OF ATTACK FROM 0 DEGREE TO 90 DEGREE FOR A MODEL WITH A LOW-ASPECT-RATIO UNSWEPT WING AND TWO DIFFERENT FUSELAGE FOREBODIES / .- Nasa, Washington, D.C., 1959 .- 25 .
Bound With Nasa Memo 1-15-59l-20,23-31 Lack No.1-18-59l-1-19-59l,1-21-59l,1-28-59l-1-29-59l
Copy Details:
Acc. No.: TR17736, Full Call No.: NASA MEMO 1-22-59L, Item type: Technical Report , Location: General Stacks,
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