Search

Advanced search

Normal view MARC view ISBD view

A THEORETICAL ANALYSIS OF A SIMPLE AERODYNAMIC DEVICE TO IMPROVE THE LONGITUDINAL DAMPING OF A CRUIFORM MISSILE CONFIGURATION AT SUPERSONIC SPEEDS

By: Clements,James B.

Material type: materialTypeLabel

materialTypeLabel

BookPublisher: 1957Description: 36.DDC classification: NACA | RM-L55H31

average rating: 0.0 (0 votes)

Holdings ( 1 )
Title notes
Comments ( 0 )

Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NACA RM-L55H31 (Browse shelf)	Not for loan		TR3501

Total holds: 0

Browsing PK Kelkar Library, IIT Kanpur Shelves , Collection code: General Stacks Close shelf browser

Previous								Next
Previous	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	NACA TM 1425 ON THE CALCULATION OF SHALLOW SHELLS	Next

Bound With Naca Rm L53a07

There are no comments for this item.

Log in to your account to post a comment.

Powered by Koha