Correlation of aerodynamic stability and control derivatives obtained from flight tests and wind tunnel tests on the XC-142A airplane

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049 ‡aMAIN
086 0 ‡aD 301.45/46-2: 68-167
100 1 ‡aBlack, Ernest L., ‡eauthor.
245 1 0 ‡aCorrelation of aerodynamic stability and control derivatives obtained from flight tests and wind tunnel tests on the XC-142A airplane / ‡cErnest L. Black, George C. Booth.
264 1 ‡aWright-Patterson Air Force Base, Ohio : ‡bAir Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, ‡c1969.
300 ‡axv, 181 pages : ‡billustrations, figures, tables ; ‡c28 cm
336 ‡atext ‡btxt ‡2rdacontent
337 ‡aunmediated ‡bn ‡2rdamedia
338 ‡avolume ‡bnc ‡2rdacarrier
490 0 ‡aAir Force Flight Dynamics Laboratory (U.S.). Technical Report ; ‡vAFFDL-TR-68-167
500 ‡a"This research and development program was performed by the Vought Aeronautics Division of the LTV Aerospace Corporation, Air Force Contract No. AF 33(615)-2987. This project was initiated under Project 8219, task 821907."
500 ‡a"Vought Aeronautics Division, LTV Aerospace Corporation."
500 ‡a"April 1969."
504 ‡aIncludes bibliographicsl references (pages 179-181).
538 ‡aMode of access: Internet.
583 1 ‡awill digitize ‡c20200915 ‡zQueued for digitization ‡cSeptember 15, 2020 ‡5miu ‡2pda
650 0 ‡aWind tunnel testing.
650 0 ‡aFlight testing.
650 0 ‡aAerodynamics.
700 1 ‡aBooth, George C., ‡eauthor.
710 2 ‡aAir Force Flight Dynamics Laboratory (U.S.), ‡eissuing agency.
710 2 ‡aLTV Aerospace Corporation, ‡esponsor.
730 0 ‡aTechnical Report Archive & Image Library (TRAIL)
899 ‡a39015095298884
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