Normal view MARC view ISBD view

EFFECTS OF INCREASED LEADING-EDGE THICKNESS ON PERFORMANCE OF A TRANSONIC ROTOR BLADE.

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1973Description: 55.DDC classification: NASA | TN D-7489

average rating: 0.0 (0 votes)

Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TN D-7489 (Browse shelf)	Not for loan		TR13993

Total holds: 0

Previous								Next
Previous	NASA TN D-7486 EXPERIMENTAL AND ANALYTICAL STUDY OF A CONICALLY DIFUSED FLOW WITH A NEARLY SEPARATED BOUNDARY LAYER.	NASA TN D-7487 FORTRAN PROGRAM FOR PREDICATING OFF-DESIGN PERFORMANCE OF CENTRIFUGAL COMPRESSORS.	NASA TN D-7488 THERMODYNAMICS AND TRANSPORT PROPERTIES OA AIR AND ITS PRODUCTS OF COMBUSTION WITH ASTM-A-.1 FUEL AND NATURAL GAS AT 20,30 AND 40 ATMOSPHERES.	NASA TN D-7489 EFFECTS OF INCREASED LEADING-EDGE THICKNESS ON PERFORMANCE OF A TRANSONIC ROTOR BLADE.	NASA TN D-7491 FLUTTER OF ELASTICALLY SUPPORTED ORTHOTROPIC PANELS INCLUDING THE EFFECTS OF FLOW ANGLE	NASA TN D-7492 GAS FLOW ANALYSIS DURING THERMAL VACUUM TEST OF A SPACECRAFT	NASA TN D-7493 UPPER TROPOSPHERIC DYNAMICS AS REFLECTED IN NIMBUS-4 THIR 6.7- UM DATA	Next

Bound With Nasa Tn D-7481-7488,Lack No 7481.

There are no comments for this item.

PKK Library