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Inlet sensitivity study for a supersonic transport

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BookSeries: NASA TN D-3881. Publisher: Washington NASA 1967Description: various pagings.Subject(s): Supersonic Transport

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Item type	Current location	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	NASA TN D-3881 (Browse shelf)	Not for loan		83109

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Previous	NASA TN D-3878 EFFECTIVENESS OF FLEXIBLE AND RIGID RING BAFFLRS FOR DAMPING LIQUID OSCILATIONS IN LARGE-SCALE CYLINDERICAL TANKS.	NASA TN D-3879 INVESTIGATION OF FATIGUE CRACK GROWTH IN TI-8A1-1M0-1V (DUPLEX-ANNEALED) SPECIMENS HAVING VARIOUS WIDTHS.	NASA TN D3880 PLASMA STABILITY AND THE BOHR-VAN LEEUWEN THEOREM.	NASA TN D-3881 Inlet sensitivity study for a supersonic transport	NASA TN D-3891 Automatically controlled air spring suspension sustem for vibration testing	NASA TN D-3892 CONTRIBUTION OF DOWNSTREAM STATOR TO THE INTERACTION NOISE OF SINGLE-STAGE AXIAL-FLOW COMPRESSOR	NASA TN D-3893 A NUMERICAL METHOD FOR DETERMINING THE AEROELASTIC DIVERGENCE CHARACTERISTICS OF UNGUIDED, SLENDER-BODY, MULTISTAGE LAUNCH VEHICLES	Next

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