Normal view MARC view ISBD view

AERODYNAMIC CHARACTERISTICS OF A SWEPT-WING CRUISE MISSILE AT MACH NUMBERS FROM 0.50 TO 2.86

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1972Description: 40.DDC classification: NASA | TN D-7069

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-7069 (Browse shelf)	Not for loan		TR12752

Total holds: 0

Previous								Next
Previous	NASA TN D-7066 EVALUATION OF AN AEROELASTIC MODEL TECHNIQUE FOR PREDICTING AIRPLANE BUFFET LOADS	NASA TN D-7067 AN ACTUATOR EXTENSION TRANSFORMATION FOR A MOTION SIMULATOR AND AN INVERSE TRANSFORMATION APPLYING NEWTON-RAPHSON'S METHODS	NASA TN D-7068 NUMERICAL METHOD FOR THE SOLUTION OF LARGE SYSTEMS OF DIFFERENTIAL EQUATIONS OF THE BOUNDARY-LAYER TYPE	NASA TN D-7069 AERODYNAMIC CHARACTERISTICS OF A SWEPT-WING CRUISE MISSILE AT MACH NUMBERS FROM 0.50 TO 2.86	NASA TN D-707 STRUCTURE AND DESIGN CONSIDERATIONS OF THE VANGUARD SLV-5 MAGNETIC FIELD SATELLITE	NASA TN D-7071 LOW-SPEED AERODYNAMIC CHARACTERISTICS OF AN AIRFOIL OPTIMIZED FOR MAXIMUM LIFT COEFFICIENT.	NASA TN D-7072 EFFECTS OF FUEL NOZZLE DESIGN ON PERFORMANCE OF AN EXPERIMENTAL ANNULAR COMBUSTOR USING NATURAL GAS FUEL.	Next

Bound With Nasa Tn D-7060-7068

There are no comments for this item.

PKK Library