The achievement of flight with manned, powered, heavier-than-air aircraft in 1903 marked the beginning of a new era in the means of transportation. A special advantage for aircraft was in speed. However, when an aircraft penetrates the air at very high speeds, the disturbed air is compressed and there are changes in the density, pressure and temperature of the air. These compressibility effects change the aerodynamic characteristics of an aircraft and introduce problems in drag, stability and control. Many aircraft designed in the post-World War II era were plagued with the effects of compressibility. Accordingly, the study of the aerodynamic behavior of aircraft, spacecraft and missiles at high-speed became a major part of the research activity of the NACA/NASA. The intent of the research was to determine the causes and provide some solutions for the aerodynamic problems resulting from the effects of compressibility. The purpose of this paper is to review some of the high-speed aerodynamic research work conducted at the Langley Research Center from the viewpoint of the author who has been active in much of the effort.


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    Title :

    Lessons Learned in the High-Speed Aerodynamic Research Programs of the NACA/NASA


    Contributors:

    Conference:

    43rd AIAA Aerospace Sciences Meeting and Exhibit ; 2005 ; Reno, NV, United States


    Publication date :

    2004-01-01


    Type of media :

    Preprint


    Type of material :

    No indication


    Language :

    English


    Keywords :



    Lessons Learned in the High-Speed Aerodynamic Research Programs of the NACA/NASA

    Spearman, M. L. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2005




    HIGH-SPEED AERODYNAMIC RESEARCH AT THE NACA/NASA LANGLEY RESEARCH CENTER

    Spearman, M. L. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2004