Search

Advanced search

Normal view MARC view ISBD view

Comparison of three methods for calculation of helicopter rotor blade loading and stresses due to stall [NASA TN D-7833]

By: Johnsan,Wayne.

Series: National Aeronaitics and Space Adminstration ; NASA Technical Note. Publisher: Wahington.D. C. National Aeronaitics and Space Adminstration 1974Description: 21p.Subject(s): Helicopter rotor blade

average rating: 0.0 (0 votes)

Holdings ( 1 )
Title notes
Comments ( 0 )

Item type	Current location	Collection	Call number	Vol info	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		NASA TN D 7831-7835	Not for loan		TR002571

Total holds: 0

Browsing PK Kelkar Library, IIT Kanpur Shelves , Collection code: COMPACT STORAGE (BASEMENT) Close shelf browser

Previous								Next
Previous	A fortan program for determining aircraft stability and control derivatives from flight data [NASA TN D -7831]	25- Mb sounding data and synoptic charts for NASA's ave ii pilot experiment[NASA TN D-7832]	Weak incident shock interactions with mach 8 laminar boundary layers [NASA TN D -7835]	Comparison of three methods for calculation of helicopter rotor blade loading and stresses due to stall [NASA TN D-7833]	Application of parameter identification technique to a hingeless helicopter rotor[NASA TN D -7834]	Pressure distributions on two-dimensional sharp-leading-edge flat plates with sweep angles of 0 degree,30 degree,and 45 degree at a mach number of 6 and angles of attack from 0 degree to 90 degree[NASA TN D-1371]	Heat- transfer and pressure measurements on a flat-plate surface and heat-transfer measurements on attached protuberances layer at mach numbers of 2.56, 3.51 and 4.44 [NASA TN D-1372]	Next

Bound vol. contains D 7831- 7835

There are no comments for this item.

Log in to your account to post a comment.

Powered by Koha