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COMPARISON OF FLIGHT-MEASURED HELICOPTER ROTOR-BLADE CHORDWISE PRESSURE DISTRIBUTIONS WITH STATIC TWO-DIMENSIONAL AIRFOIL CHRACTERISTICS.

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BookPublisher: Nasa, Washington, D.C. 1967Description: 54.DDC classification: NASA | TN D-3936

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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-3936 (Browse shelf)	Not for loan		TR11987

Total holds: 0

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Previous	NASA TN D-3933 THE STRUCTURE OF AN ATMOSPHERE FROM ON-BOOARD MEASUREMENTS OF PRESSURE,TEMPERATURE,AND ACCELERATION.	NASA TN D-3934 ANALYSIS OF SELF-LOCAMOTIVE PERFORMANCE OF LUNAR EXPOLRERS BASED ON EXPERIMENTAL REDUCED-GRAVITY STUDIES.	NASA TN D-3935 MODELS FOR THE ANALYSIS OF CN VIOLET RADIATION BEHIND SHOCK WAVES IN AIR CONTAMINATED WITH CARBON-BEARING COMPOUNDS.	NASA TN D-3936 COMPARISON OF FLIGHT-MEASURED HELICOPTER ROTOR-BLADE CHORDWISE PRESSURE DISTRIBUTIONS WITH STATIC TWO-DIMENSIONAL AIRFOIL CHRACTERISTICS.	NASA TN D-3937 EXPERIMENTAL STUDY OF THE APPLICATION OF THE PENETROMETER TECHNIQUE TO THE LUNAR SURVEYING STAFF CONCEPT.	NASA TN D-3938 GROUND EFFECTS ON A FOUR-PROPELLER TILT-WING CONFIGURATION OVER A FIXED AND A MOVING GROUND PLANKE.	NASA TN D-3939 APPLICATION OF COMPUTERS TO THE FORMULATION OF PROBLEMS IN CURVILINEAR COORDATE SYSTEMS.	Next

Bound With Nasa Tn D-3931-3935,3937-40.

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