Normal view MARC view ISBD view

EXPERIMENTAL INVESTIGATION OF SOME OF THE PARAMETERS RELATED TO THE STABILITY AND CONTROL OF AERIAL VEHICLES SUPPORTED BY DUCTED FANS

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1960Description: 34.DDC classification: NASA | TN D-616 -

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-616 - (Browse shelf)	Not for loan		TR10231

Total holds: 0

Previous								Next
Previous	NASA TN D-6156 FTIGUE LIVES AT 600 DEGHREE OF 120-MILLIMETER-BORE BALL BEARINGS OF AISI M-50,AISI M-1,AND WB-49 STEELS.	NASA TN D-6157 ANALYTICAL HEAT TRANSFER INVESTIGATION OF INSULATED LIQUID METHANE FUSELAGE TANKS FOR SUPERSONIC CRUISE AIRCRAFT.	NASA TN D-6159 HYDRODYNAMIC ENTRANCE EFFECT ON BOILING HAD NEAR CRIRICAL HYDROGEN HEAT TRANSFER.	NASA TN D-616 - EXPERIMENTAL INVESTIGATION OF SOME OF THE PARAMETERS RELATED TO THE STABILITY AND CONTROL OF AERIAL VEHICLES SUPPORTED BY DUCTED FANS	NASA TN D-6161 COMPUTER PROGRAM FOR PRELIMINARY DESIGN AND ANALYSIS OF V/STOL TIP-TURBINE FANS	NASA TN D-6162 SOME CHARACTERISTICS OF A BOILING-WATER-COOLED VAPOR TRANSPORT FUEL PIN	NASA TN D-6163 EXPERIMENTAL PERFORMANCE AND COMBUSTION STABILITY OF A FULL-SCALE DUCT DURNER FOR A SUPERSONIC TURBOFAN ENGINE	Next

Bound With Nasa Tn D-611-20

There are no comments for this item.

PKK Library