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Flight investigation of XB-70 structural response to oscillatory aerodynamic shaker excitation and correlation with analytical results

By: James M Mckay.

Contributor(s): John H Wykes.

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BookPublisher: DDC classification: NASA | TN D-7227 -

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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-7227 - (Browse shelf)	Not for loan		TR9443

Total holds: 0

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Previous	NASA TN D-7224 - Electron avalanche structure determined by random walk theory	NASA TN D-7225 - Evaluation of an experimental short-length annular combustor	NASA TN D-7226 - Measurements of surface-pressure fluctuations on the XB-70 airplane at lacal mach numbers up to 2.45	NASA TN D-7227 - Flight investigation of XB-70 structural response to oscillatory aerodynamic shaker excitation and correlation with analytical results	NASA TN D-7228 - Method for estimating static aerodynamic characteristics for slender bodies of circular and noncircular cross section alone and with lifting surfaces at angles of attack from 0(degree) to 90(degree)	NASA TN D-7229 - Analytical evaluation of jet noise source lacation technique utilizing an acoustically hard baffle with aperture	NASA TN D-7232 - ADHESION, FRICTION, AND WEAR OF A COPPER BICRYSTAL WITH (111) AND (210) GRAINS	Next

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