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Flugmechanik
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Wing pressure distributions from subsonic tests of a high-wing transport model
Wing planform effects at supersonic speeds for an advanced fighter configuration
Wing-alone aerodynamic characteristics for high angles of attack of supersonic speeds
Wing aerodynamic loading caused by jet-induced lift associated with STOL-OTW configurations
Wind tunnel wall effects in V/STOL model testing Final report, 1 Oct. 1965 - 31 Mar. 1967
Wind tunnel tests on a tail-less swept wing span-distributed cargo aircraft configuration
Wind tunnel tests of a wing installed model VTOL lift fan with coaxial drive turbine
Wind tunnel test on a 1/4.622 Froude scale, hingeless rotor, tilt rotor model, volume 4
Wind tunnel test on a 1/4.622 Froude scale, hingeless rotor, tilt rotor model, volume 3