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  • Other Sources  (18)
  • 1
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    Handling qualities of light aircraft with advanced control systems and displays (1971)
    In:  CASI
    Details
    Publication Date: 2005-11-27
    Description: Flight tests to determine handling qualities of general aviation aircraft during ILS approaches in turbulent air
    Keywords: AIRCRAFT
    Type: NASA AIRCRAFT SAFETY AND OPERATING PROBL., VOL. 1 1971; P 189-206
    Format: text
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    NASA TECHNICAL REPORTS
  • 2
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    KC-135 winglet program overview (1982)
    In:  CASI
    Details
    Publication Date: 2006-02-14
    Description: A joint NASA/USAF program was conducted to accomplish the following objectives: (1) evaluate the benefits that could be achieved from the application of winglets to KC-135 aircraft; and (2) determine the ability of wind tunnel tests and analytical analysis to predict winglet characteristics. The program included wind-tunnel development of a test winglet configuration; analytical predictions of the changes to the aircraft resulting from the application of the test winglet; and finally, flight tests of the developed configuration. Pressure distribution, loads, stability and control, buffet, fuel mileage, and flutter data were obtained to fulfill the objectives of the program.
    Keywords: AERODYNAMICS
    Type: KC-135 Winglet Program Rev.; p 1-46
    Format: text
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    NASA TECHNICAL REPORTS
  • 3
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    A flight evaluation of curved landing approaches (1972)
    In:  CASI
    Details
    Publication Date: 2006-03-27
    Description: The development of STOL technology for application to operational short-haul aircraft is accompanied by the requirement for solving problems in many areas. One of the most obvious problems is STOL aircraft operations in the terminal area. The increased number of terminal operations needed for an economically viable STOL system as compared with the current CTOL system and the incompatibility of STOL and CTOL aircraft speeds are positive indicators of an imminent problem. The high cost of aircraft operations, noise pollution, and poor short-haul service are areas that need improvement. A potential solution to some of the operational problems lies in the capability of making curved landing approaches under both visual and instrument flight conditions.
    Keywords: AIRCRAFT
    Type: STOL Technol.; p 245-258
    Format: text
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    NASA TECHNICAL REPORTS
  • 4
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    Handling quality evaluation of seven general aviation aircraft. (1966)
    In:  Other Sources
    Details
    Publication Date: 2011-08-11
    Description: Handling quality evaluation of seven general aviation aircraft of type operated under instrument flight conditions
    Keywords: AIRCRAFT
    Type: /SOCIETY OF EXPERIMENTAL TEST PILOTS
    Format: text
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    NASA TECHNICAL REPORTS
  • 5
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    Recent wake turbulence flight test programs (1974)
    In:  Other Sources
    Details
    Publication Date: 2011-08-16
    Description: In early flight tests the size and intensity of the wake vortexes generated by aircraft ranging in size from the Learjet to the C-5A and the B-747 were studied to determine the effects of aircraft configuration, weight, and speed. Early problems were related to vortex marking, the measurement of separation distance, and test techniques. Recent tests conducted with B-747 showed that vortexes were alleviated by reducing the deflection of the outboard flaps. It was found that a more rapid dissipation of the vortex system can be obtained through alterations in the span lift distribution.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Format: text
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    NASA TECHNICAL REPORTS
  • 6
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    Wake vortex attenuation flight tests - A status report (1982)
    In:  Other Sources
    Details
    Publication Date: 2011-08-18
    Description: (Previously announced in STAR as N81-19057)
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Format: text
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    NASA TECHNICAL REPORTS
  • 7
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    Vortex attenuation flight experiments (1977)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Description: Flight tests evaluating the effects of altered span loading, turbulence ingestion, combinations of mass and turbulence ingestion, and combinations of altered span loading turbulance ingestion on trailed wake vortex attenuation were conducted. Span loadings were altered in flight by varying the deflections of the inboard and outboard flaps on a B-747 aircraft. Turbulence ingestion was achieved in flight by mounting splines on a C-54G aircraft. Mass and turbulence ingestion was achieved in flight by varying the thrust on the B-747 aircraft. Combinations of altered span loading and turbulence ingestion were achieved in flight by installing a spoiler on a CV-990 aircraft and by deflecting the existing spoilers on a B-747 aircraft. The characteristics of the attenuated and unattenuated vortexes were determined by probing them with smaller aircraft. Acceptable separation distances for encounters with the attenuated and unattenuated vortexes are presented.
    Keywords: AERODYNAMICS
    Type: Wake Vortex Minimization; p 369-403
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 8
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    Wake vortex technology (1978)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Description: A brief overview of the highlights of NASA's wake vortex minimization program is presented. The significant results of this program are summarized as follows: (1) it is technically feasible to reduce significantly the rolling upset created on a trailing aircraft; (2) the basic principles or methods by which reduction in the vortex strength can be achieved have been identified; and (3) an analytical capability for investigating aircraft vortex wakes has been developed.
    Keywords: AERODYNAMICS
    Type: CTOL Transport Technol., 1978; p 757-771
    Format: application/pdf
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  • 9
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    An evaluation of the handling qualities of seven general-aviation aircraft (1966)
    In:  CASI
    Details
    Publication Date: 2019-05-30
    Description: Handling qualities and stability and control characteristics of general-aviation aircraft
    Keywords: AIRCRAFT
    Type: NASA-TN-D-3726
    Format: application/pdf
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  • 10
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    An evaluation of general aviation aircraft flying qualities. (1966)
    In:  Other Sources
    Details
    Publication Date: 2019-05-30
    Description: Flying qualities of six late-model personal-owner aircraft in visual and instrument flight
    Keywords: AIRCRAFT
    Type: SAE PAPER 660219
    Format: text
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    NASA TECHNICAL REPORTS
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