by National Aeronautics and Space Administration, Scientific and Technical Information Office, For sale by the National Technical Information Service] in Washington, D.C, [Springfield, Va .
Written in English
|Statement||Terrell W. Feistel ; Joseph P. Morelli.|
|Series||NASA technical paper -- 1696., AVRADCOM technical memorandum -- 80-A-1.|
|Contributions||Morelli, Joseph P., United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., Aeromechanics Laboratory.|
|The Physical Object|
|Pagination||iii, 52 p. :|
|Number of Pages||52|
LARGE-SCALE WIND-TUNNEL TESTS OF A DEFLEETED SLIPS= STOL MODEL WITH WINGS OF VARIOUS ASPECT RATIOS By V. Robert Page, Stanley 0. Dickinson, and Wallace H. Deckert Ames Research Center A wind-tunnel investigation was conducted to determine the longitudinal force characteristics of a large-scale model representative of a propeller- driven STOL Author: Kirtlano Afb, N Mex. Feistel, , describes a wind tunnel model of a twin-engine airplane (airplane) with wing-mounted engines, noting that "The propellers were contrarotating and propeller rotation was down inboard for . Wind tunnel tests of wing stall, performance, and longitudinal stability & control of large model v/stol tilt wing transport aircraft Addeddate Large-scale wind-tunnel tests of an airplane model with a 45 degree sweptback wing of aspect ratio employing high-velocity blowing over the leading- and trailing-edge flaps One of 5, reports in the series: NACA Research Memorandums available on this by: 4.
Full-scale testing in a wind tunnel is only possible with small aircraft - see the answers to this question for examples. Even then, the speeds do not match the top speed of the aircraft, so the loads are a fraction of the real loads. Jan Roskam observes in his book "Roskam's airplane war stories". Large-scale wind-tunnel investigation of an airplane model with a tilt wing of aspect ratio , and four propellers, in the presence of a ground plane by Deckert, W. H. ; Dickinson, S. O. ; Page, V. R. Large-scale wind-tunnel tests of inverting flaps on a STOL utility aircraft model / (Washington, D.C.: National Aeronautics and Space Administration, Scientific and . University of Oklahoma Libraries. Services. Navigate; Linked Data; Dashboard; Tools / Extras; Stats; Share. Social. Mail.
A Wind Tunnel Test of the Full Scale Boeing Multi-Functional Aircraft Inlet Dale M. Pitt, James P. Dunne, Edward V. White The Boeing Company. Wind tunnel experiments with scaled model turbines are a viable complement to field tests and simulations. The scaling of a 5 MW reference turbine with the aim of maintaining the design tip speed. The large size of commercial aircraft relative to existing icing wind tunnels and lack of robust scaling methods also makes ice accretion wind tunnel testing difficult. Hybrid or truncated airfoil models use full-scale leading edges with redesigned aft sections to provide test articles with much reduced model chord and therefore tunnel blockage Cited by: 3. NASA recently tested a full-sized tail from a commercial aircraft that was modified and equipped with tiny jets called "sweeping jet actuators" to blow air across the rudder surfaces.