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Large-scale tests of an airplane model with a double-delta wing, including longitudinal and lateral characteristics and ground effectsAerodynamic characteristics and ground effects of supersonic transport with double delta wing
Document ID
19690011658
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Corsiglia, V. R. (NASA Ames Research Center Moffett Field, CA, United States)
Koenig, D. G. (NASA Ames Research Center Moffett Field, CA, United States)
Morelli, J. P. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1969
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-5102
Accession Number
69N21020
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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