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COMPRESSIBLE-FLOW SOLUTIONS FOR THE ACTUATOR DISK

By: Delano,James B.

Contributor(s): Crigier,John L.

Material type: materialTypeLabel

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BookPublisher: 1953Description: 70.DDC classification: NACA | RM-L53A07

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NACA RM-L53A07 (Browse shelf)	Not for loan		TR3590

Total holds: 0

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Previous	NACA 498 IMPROVED AIRPLANE WINDSHIELDS TO PROVIDE VISION IN STORARY WEATHER	NACA 499 WIND-TUNNEL RESEARCH COMPARING LATERAL CONTROL DEVICES,PARATICULARY AT HIGH ANGLES OF ATTACK.	NACA 500 THE INFLUENCE OF TIP SHAPE ON THE WING LOAD DISTRIBUTION AS DETERMIND BY FLYIGHT TESTS	NACA RM-L53A07 COMPRESSIBLE-FLOW SOLUTIONS FOR THE ACTUATOR DISK	NACA RM-L55H31 A THEORETICAL ANALYSIS OF A SIMPLE AERODYNAMIC DEVICE TO IMPROVE THE LONGITUDINAL DAMPING OF A CRUIFORM MISSILE CONFIGURATION AT SUPERSONIC SPEEDS	NACA TM 1423 SAFEGUARDS AGAINST FLUTTER OF AIRPLANES	NACA TM 1424 ON THE THEORY OF ANISOTROPIC SHALLOW SHELLS	Next

Bound With Naca Rm L55h31

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