NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Matrix method of determining the longitudinal-stability coefficients and frequency response of an aircraft from transient flight data
Document ID
19930083297
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Donegan, James J
Pearson, Henry A
Date Acquired
August 29, 2013
Publication Date
June 1, 1951
Report/Patent Number
NACA-TN-2370
Report Number: NACA-TN-2370
Accession Number
93R12587
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available