NASA / TM X-179 -
Fournier,Paul G
WIND-TUNNEL INVESTIGATION AT HIGH SUBSONIC SPEED OF THE STATIC LONGITUDINAL STABILITY CHARACTERISTICS OF A WINGED REENTRY VEHICLE HAVING A LARGE NEGATIVELY DEFLECTED FLAP-TYPE CONTROL SURFACE
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.- Nasa, Washington, D.C., 1959
.- 21 .
Bound With Nasa Tm X-165-79
Copy Details:
Acc. No.: TR8836, Full Call No.: NASA TM X-179 -, Item type: Technical Report , Location: General Stacks,
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