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EXPERIMENTAL INVESTIGATION OF THE CORNERING CHARACTERISTICS OF A C40 X 14-21 CANTILEVER AIRCRAFT TIRE

By: Dreher,Robert C.

Contributor(s): Tanner,John A.

Material type: materialTypeLabel

materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1973Description: 21.DDC classification: NASA | TN D-7203

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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-7203 (Browse shelf)	Not for loan		TR14760

Total holds: 0

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Previous	NASA TN D-720 EFFECT OF RATIO OF JET AREA TO TOTAL AREA AND OF PRESSURE RATIO ON LIFT AUGMENTATION OF ANNULAR JETS IN GROUND EFFECT UNDER STATIC CONDITIONS	NASA TN D-7201 ANALYTICAL STUDY OF THE PERFORMANCE OF A GUST ALLEVIATION SYSTEM FOR A STOL AIRPLANE	NASA TN D-7202 FLIGHT-MEASURED BASE PRESSURE COEFFICIENTS FOR THICK BOUNDARY-LAYER FLOW OVER AN AFT-FACING STEP FOR MACH NUMBERS FROM 0.4 TO 2.5	NASA TN D-7203 EXPERIMENTAL INVESTIGATION OF THE CORNERING CHARACTERISTICS OF A C40 X 14-21 CANTILEVER AIRCRAFT TIRE	NASA TN D-7204 DESIGN AND EVALUATION OF AN OPTICAL FINE-POINTING CONTROL SYSTEM FOR TELESCOPES UTILIZING A DIGITAL STAR SENSOR	NASA TN D-7205 EFFECT OF WING ASPECT RATIO AND FLAP SPAN ON AERODYNAMIC CHARACTERISTICS OF AN EXTERNALLY BLOWN JET-FLAP STOL MODEL	NASA TN D-7206 FRICTION, WEAR, AND TRANSFER OF CARBON AND GRAPHITE TO COPPER, CHROMIUM, AND ALUMINUM METAL SURFACES IN VACUUM	Next

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