Search

Advanced search

Normal view MARC view ISBD view

Aerodynamic stability and performance characteristics obtained from autopilot-controlled supersonic test vehicles

By: E T Marley.

Material type: materialTypeLabel

materialTypeLabel

BookPublisher: DDC classification: NATO | AGARD R-379

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	NATO AGARD R-379 (Browse shelf)	Not for loan Untraceable		TR16610

Total holds: 0

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

Previous								Next
Previous	NATO AGARD R-376 Techniques for the investigation of aerodynamic heating effects in free flight	NATO AGARD R-377 Techniques de measure de l'echauffement cinetique A L'Aide DU Missile 'Antares'	NATO AGARD R-378 Measurements of dynamic stability from three simplified free-flight models of a supersonic research aircraft (Briston ER. 134) over the mach number range 1.2 -2.6	NATO AGARD R-379 Aerodynamic stability and performance characteristics obtained from autopilot-controlled supersonic test vehicles	NATO AGARD R-380 Measurement of aerodynamic characteristics of re-entry configurations in free flight at hypersonic and near-orbital speeds	NATO AGARD R-391 ASCENT PROBLEMS OF SOUNDING ROCKETS	NATO AGARD R-392 EFFICACITE DE DIFFERENTS PROCEDES POUR REDUIRE LA DISPERSION DES MISSILES EXPERIMENTAUX	Next

There are no comments for this item.

Log in to your account to post a comment.

Powered by Koha