This paper presents a summary of results obtained in dynamic tests of free-flight models of various configurations suitable for V/STOL transport aircraft at the NASA Langley Research Center. The configurations covered will be the tilt-wing propeller-driven type as represented by the XC-142A tri-service transport, the fan-in-wing type as represented by the XV-5A research airplane, and the jet-lift type as represented by the Dornier 00-31 transport. The test techniques themselves are not described in this paper since they have been described in detail previously in references 1 and 2.
Dynamic Tests of V/STOL Transport Models
AIAA Transport Aircraft Design and Operations Meeting ; 1964 ; Seattle, WA, US
1964-08-10
Aufsatz (Konferenz)
Keine Angabe
Englisch
Dynamic tests of v/stol transport models
NTRS | 1964
|Dynamic tests of v/stol transport models
AIAA | 1964
|STOL-V/STOL City Center Transport Aircraft Study
NTIS | 1964
Flight tests under IFR with an STOL transport aircraft
TIBKAT | 1968
|NTRS | 1967
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