Welcome to P K Kelkar Library, Online Public Access Catalogue (OPAC)

Normal view MARC view ISBD view

WIND TUNNEL INVESTIGATION OF TAIL BUFFET AT SUBSONIC AND TRANSONIC SPEEDS EMPLOYING A DYNAMIC ELASTIC AIRCRAFT MODEL.[NASA TN D-1362]

By: Rigby, R. N.
Contributor(s): Cornette, E. S.
Material type: materialTypeLabelBookSeries: National Aeronautics and Space Administration ; NASA Technical Note. Publisher: Washington, D.C. National Aeronautics and Space Administration 1962Description: 43p.
    average rating: 0.0 (0 votes)
Item type Current location Collection Call number Status Date due Barcode Item holds
Technical Report Technical Report PK Kelkar Library, IIT Kanpur
General Stacks NASA TN D-1362 (Browse shelf) Not for loan TR7458
Total holds: 0

Bounds With NASA TN D 1361-1370

There are no comments for this item.

Log in to your account to post a comment.

Powered by Koha