3/4 front view offull scale X-22A ducted fan model. Chuck Greco

MSC 040A Space Shuttle: 11ft. W.T. Tests pf Acoustic Environment (Configuration 5 with James M. Peterson

XV-5A airplane installed in 40x80ft Subsonic Wind Tunnel at NASA Ames Research Center with Tom Mills. The propulsive lift system was tested to determine power-on performance characteristics in preparation for flight tests.

AVROCAR Annular Jet VTOL Airplane; 40x80ft w.t. tests

HYPERVELOCITY BALLISTICS RANGE (HBR) IMPACT CHAMBER, HI SPEED FARAMING CAMERA & STATIONS

M2-F2 lifting body flight vehicle in 40x80ft w.t.

XV-5A airplane installed in 40x80ft Subsonic Wind Tunnel at NASA Ames Research Center with Tom Mills. The propulsive lift system was tested to determine power-on performance characteristics in preparation for flight tests. Used in Memoiors of an Aeronautical Engineer, Flight Tests at Ames Research Center 1940-1970 NASA-SP-2002-4526 (Seth B. Anderson)

3/4 front view of full scale X-22A ducted fan model. Chuck Greco

5 Degree Freedom of Motion Simulator with R. Gerdes (delayed exposure using lights to show motion)

3/4 front view of full scale X-22A ducted fan model. Chuck Greco

XV-5A airplane installed in 40x80ft Subsonic Wind Tunnel at NASA Ames Research Center with Tom Mills. The propulsive lift system was tested to determine power-on performance characteristics in preparation for flight tests.

Boeing 737 Aerodynamics in Air and Freon 12ft w.t. test-12-495

V/STOL Lift -cruise fan transport with Stan Dickenson in 40 x 80 ft. W. T.