Search

Advanced search

Normal view MARC view ISBD view

FREE-FLIGHT INVESTIGATION OF THE DEPLOYMENT, DYNAMIC STABILITY, AND CONTROL CHARACTERISTICS OF A 1/12-SCALE DYNAMIC RADIO-CONTROLLED MODEL OF A LARGE BOOSTER AND PARAWING

By: Burk,Jr.,Sanger M.

Material type: materialTypeLabel

materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1963Description: 19.DDC classification: NASA | TN D-1932 -

average rating: 0.0 (0 votes)

Holdings ( 1 )
Comments ( 0 )

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-1932 - (Browse shelf)	Not for loan		TR10206

Total holds: 0

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

Previous								Next
Previous	NASA TN D-1918 ON ISOMETRIC DEFORMATION OF SCREW SURFACES	NASA TN D-1919 A CONTRIBUTION TO THE THEORY OF PRESSURE STABILIZED STRUCTURES	NASA TN D-1920 ANALYSIS OF AXISYMMETRIC,ROTATING PRESSURIZED FILAMENTARY STRUCTURES	NASA TN D-1932 - FREE-FLIGHT INVESTIGATION OF THE DEPLOYMENT, DYNAMIC STABILITY, AND CONTROL CHARACTERISTICS OF A 1/12-SCALE DYNAMIC RADIO-CONTROLLED MODEL OF A LARGE BOOSTER AND PARAWING	NASA TN D-1933 - EFFECT OF FABRICATION-TYPE SURFACE ROUGHNESS ON TRANSITION ON OGIVE-CYLINDER MODELS AT MACH NUMBERS OF 1.61 AND 2.01	NASA TN D-1934 - INVESTIGATION OF THE LANDING CHARACTERISTICS OF A REENTRY VEHICLE HAVING CANTED MULTIPLE-AIR-BAG LOAD-ALLEVIATION SYSTEM	NASA TN D-1935 - LOADS INDUCED ON A FLAT PLATE AT A MACH NUMBER OF 4.5 WITH A SONIC OR SUPERSONIC JET EXHAUSTING NORMAL TO THE SURFACE	Next

There are no comments for this item.

Log in to your account to post a comment.

Powered by Koha