Normal view MARC view ISBD view

Analytical investigation of the spin and recovery characteristics of a supersonic trainer airplane having a 24o swept wing [NASA TM X-606]

Material type: materialTypeLabel

BookSeries: National Aeronautics and Space Administration [NASA]. Publisher: Washington, D. C. NASA 1962Description: 39p.Subject(s): SupersonicDDC classification: NASA | TM X-606

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	Reference	NASA TM X-606 (Browse shelf)	Not for loan		102484

Total holds: 0

Previous								Next
Previous	NASA CR-2043 ACCEPTABILITY OF VTOL AIRCRAFT NOISE DETERMINED BY ABSOLUTE SUBJECTIVE TESTING[NASA CR-2043]	NASA CR-2044 APPLICATIONS OF THE THEORY OF OPTIMAL CONTROL OF DISTRIBUTED-PARAMETER SYSTEMS TO STRUCTURAL OPTIMIZATION[NASA CR-2044]	NASA CR-2045 EVALUATION OF INSULATION MATERIALS AND COMPOSITES FOR USE IN A NUCLEAR RADIATION ENVIRONMENT, PHASE I [NASA CR-2045]	NASA TM X-606 Analytical investigation of the spin and recovery characteristics of a supersonic trainer airplane having a 24o swept wing [NASA TM X-606]	NASA TN- 2472 Hypervelocity impact damage characteristics in armored space radiator tubes	NASA TN D-1281 Analytical and experimental investigation of forces and frequencies resulting from liquid [NASA TN D-1281]	NASA TN D-1525 Influence of weight parameters on the propulsion requirements of orbit-launched vehicles [NASA TN D-1525]	Next

There are no comments for this item.

PKK Library