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ACCEPTABILITY OF VTOL AIRCRAFT NOISE DETERMINED BY ABSOLUTE SUBJECTIVE TESTING[NASA CR-2043]

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Material type: Text

TextLanguage: English Series: National Aeronautics and Space Administration (NASA)Publication details: NASA 1972 Washington, D. C.Description: vi, 84pSubject(s):

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Holdings
Item type	Current library	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	Reference	NASA CR-2043 (Browse shelf(Opens below))	Not for loan		TR8072

Total holds: 0

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Previous	NASA CR-2040 ATMOSPHERIC RENDEZVOUS FEASIBILITY STUDY [NASA CR-2040]	NASA CR-2041 Effects of aircraft noises on the sleep of women [NASA CR-2041]	NASA CR-2042 EVALUATION OF INSULATION MATERIALS AND COMPOSITES FOR USE IN A NUCLEAR RADIATION ENVIRONMENT, PHASE II FINAL REPORT [ NASA CR-2042]	NASA CR-2043 ACCEPTABILITY OF VTOL AIRCRAFT NOISE DETERMINED BY ABSOLUTE SUBJECTIVE TESTING[NASA CR-2043]	NASA CR-2044 APPLICATIONS OF THE THEORY OF OPTIMAL CONTROL OF DISTRIBUTED-PARAMETER SYSTEMS TO STRUCTURAL OPTIMIZATION[NASA CR-2044]	NASA CR-2045 EVALUATION OF INSULATION MATERIALS AND COMPOSITES FOR USE IN A NUCLEAR RADIATION ENVIRONMENT, PHASE I [NASA CR-2045]	NASA TM X-606 Analytical investigation of the spin and recovery characteristics of a supersonic trainer airplane having a 24o swept wing [NASA TM X-606]	Next

Bound With NASA CR-2041-45( Bound Acc. No. 101576)

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