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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Wind tunnel tests to determine effect of angle of attack on maximum lift at stall for half-wing models, and single engine, jet propelled aircraft
Wind-tunnel tests of full scale practical configuration of lifting fan v/stol aircraft show transition pitching moments comparable to conventional aircraft, and that lift increases with greater forward speed
Wind tunnel test of dynamic stability characteristics of spherically blunted 10 degree cones
Wind tunnel techniques used to determine pitch damping at large angles of oscillation for proposed mars atmospheric entry vehicles
Large scale wind tunnel investigation of low speed aerodynamic characteristics of supersonic transport model having variable sweep wings
Wind tunnel investigations of effect on static stability of modifications to swept wing fighter aircraft model
Wind tunnel research of deep stall aerodynamic characteristics of T tail analyzed as preliminary design guide
Flight experience with Ogee wing at low speed
Wind tunnel technique for measuring frequency response of flexible airplane to vertical sinusoidal gusts
Dynamic excitation by ground winds of large Saturn type launch vehicle structures
Free flight dynamic stability measurements indicate that boundary layer transition has no perceptible effect
Wind tunnel research of deep stall aerodynamic characteristics of T tail analyzed as preliminary design guide
Simultaneous FM telemetry measurement of four aerodynamic forces acting on free flying models in wind tunnel
Grid turbulence for large Reynolds numbers, noting consistency of power spectra values with Kolmogoroff scaling, decay law and Reynolds number effect on turbulence
Full scale wind tunnel investigation of VTOL AIRCRAFT with jet ejector system for lift augmentation
Low speed static aerodynamic characteristics of three ram-air inflated low aspect ratio fabric wings
Wind tunnel technique for measuring frequency response of flexible airplane to vertical sinusoidal gusts
Power spectral density /PSD/ methods applied to prediction of aircraft responses to continuous turbulence