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FLIGHT TEST RESULTS OF TRAILING EDGE FLAP DESIGNED FOR DIRECT-LIFT CONTROL.

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BookPublisher: NATIONAL AERONAUTICS AND SPACE ADMINISTRATION, WASHINGTON, D.C. Description: ,80.DDC classification: NASA | CR-1426

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)	NASA CR-1426 (Browse shelf)	Not for loan		101489

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Previous	NASA CR-1394 HOLOGRAPHIC MICROSCOPHY FOR THE DETERMINATION OF FAILURE MECHANISMS IN MONOLITHIC CIRCUITS.	NASA CR-1406 MEASUREMENTS OF NEGATIVE ION PRODUCTION IN ATMOSPHERIC GASES	NASA CR-1421 THE TRANSIENT RESPONSE OF COUPLED ACOUSTO-MECHANICAL SYSTEMS.	NASA CR-1426 FLIGHT TEST RESULTS OF TRAILING EDGE FLAP DESIGNED FOR DIRECT-LIFT CONTROL.	NASA CR-1440 SIMPLIFIED PROCEDURES FOR ESTIMATING FLAPWISE BENDING MOMENTS ON HELICOPTER ROTOR BLADES.	NASA CR-1451 ALTERNATOR AND VOLTAGE REGULATOR-EXCITER FOR A BRAYTON CYCLE SPACE POWER SYSTEM 1- DESIGN AND DEVELOPMENT	NASA CR-1457 MANUAL FOR STRUCTURAL STABILITY ANALYSIS OF SANDWICH PLATES AND SHELLS.	Next

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