Wind-tunnel investigation of a VTOL jet-transport model with powered lift engines in pods at wing midspan or inboard /
Raymond D. Vogler.
Description
- Language(s)
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English
- Published
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Washington, DC : National Aeronautics and Space Administration, 1970.
- Summary
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Four ejectors mounted in each pod under each wing and powered with compressed air were used to simulate vertical-lift, fan-type jet engines. Data were obtained through an angle-of-attack range to show the effects of engine-pod location, ground-plane movement, flaps, tail size and location, and l0⁰ of sideslip on the aerodynamic characteristics of the model, and the effects of configuration changes on the jet and free-stream interference increments.--P. [i].
- Note
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"L-6962."
"NASA TN D-5770."
"April 1970."
Also available online in PDF from NASA Technical Reports Server Web site.
- Physical Description
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[i], 151 p. :
ill. ;
26 cm.
Viewability
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University of Illinois at Urbana-Champaign
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