NASA / CR-1926
Gunness,C.
FLOW FIELD ANALYSIS OF AIRCRAFT CONFIGURATION USING A NUMERICAL SOLUTION TO THE THREE-DIMENSIONAL UNIFIED SUPERSONIC/HYPERSONIC SMALL-DISTURBENCE EQUATIONS / .- Nasa, Washington, D.C., 1972 .- 114 .
Bound With Nasa Cr-1921-28
Copy Details:
Acc. No.: TR8346, Full Call No.: NASA CR-1926, Item type: Technical Report , Location: General Stacks,
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Gunness,C.
FLOW FIELD ANALYSIS OF AIRCRAFT CONFIGURATION USING A NUMERICAL SOLUTION TO THE THREE-DIMENSIONAL UNIFIED SUPERSONIC/HYPERSONIC SMALL-DISTURBENCE EQUATIONS / .- Nasa, Washington, D.C., 1972 .- 114 .
Bound With Nasa Cr-1921-28
Copy Details:
Acc. No.: TR8346, Full Call No.: NASA CR-1926, Item type: Technical Report , Location: General Stacks,
------------------------- --------------------- ------ --------- ------- ------- --------- --------