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AN AEROELASTIC MODEL APPROACH FOR THE PREDICTION OF BUFFET BENDING LOADS ON LAUNCH VEHICLES

Doggett, R. V., Jr., Hanson, P. W.

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AN AEROELASTIC MODEL APPROACH FOR THE PREDICTION OF BUFFET BENDING LOADS ON LAUNCH VEHICLES

Name: AN AEROELASTIC MODEL APPROACH FOR THE PREDICTION OF BUFFET BENDING LOADS ON LAUNCH VEHICLES
Author: Doggett, R. V., Jr., Hanson, P. W.

Author / Organization: Doggett, R. V., Jr., Hanson, P. W.

Aerospace & Aviation Published 2019 Verification Pending

Overview & Synopsis

Aeroelastic model approach for prediction of buffet bending loads on launch vehicles

Indexed from repository: NASA Technical Reports Server (ntrs.nasa.gov)

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Document Title	AN AEROELASTIC MODEL APPROACH FOR THE PREDICTION OF BUFFET BENDING LOADS ON LAUNCH VEHICLES
Author / Organization	Doggett, R. V., Jr., Hanson, P. W.
Subject & Discipline	OTHER
Categories	Aerospace & Aviation
Publication Year	2019
License / Rights	Public Domain / NASA STI Open Access
Resource Verification	Listed PDF (Verification Pending)
Original Host Website	NASA Technical Reports Server (`ntrs.nasa.gov`)
File Format	application/pdf (Portable Document Format)
Language	EN
Catalog ID	`DOC-73063`
Original Source Link	Visit Source Page on ntrs.nasa.gov »