RISS 학술연구정보서비스

검색
다국어 입력

http://chineseinput.net/에서 pinyin(병음)방식으로 중국어를 변환할 수 있습니다.

변환된 중국어를 복사하여 사용하시면 됩니다.

예시)
  • 中文 을 입력하시려면 zhongwen을 입력하시고 space를누르시면됩니다.
  • 北京 을 입력하시려면 beijing을 입력하시고 space를 누르시면 됩니다.
닫기
    인기검색어 순위 펼치기

    RISS 인기검색어

      ON AERODYNAMICS AND VORTICAL LAYER OF WAVERIDERS AT HYPERSONIC SPEEDS

      한글로보기

      https://www.riss.kr/link?id=A2097688

      • 0

        상세조회
      • 0

        다운로드
      서지정보 열기
      • 내보내기
      • 내책장담기
      • 공유하기
      • 오류접수

      부가정보

      다국어 초록 (Multilingual Abstract)

      The aerodynamic data of two waveriders developed by means of Hypersonic Small Disturbance Theory for two elliptic cones are presented and analyzed for a wide range of Mach numbers and angles of attack. Various off-design performances of waverider with on-design performances are obtained and fully discussed. These data about aerodynamics and performaces of waveriders containing some important information for high speed flying objects could be used for the design of a hypersonic airplane which is being investigated as a future plane. Through entropy distributions for elliptic cones and vaveriders, the vortical layer which is quite difficult to be studied especially for a special body like a waverider is handled in this paper and numerical methods to catch the vortical layer more clearly are also discussed.
      번역하기

      The aerodynamic data of two waveriders developed by means of Hypersonic Small Disturbance Theory for two elliptic cones are presented and analyzed for a wide range of Mach numbers and angles of attack. Various off-design performances of waverider with...

      The aerodynamic data of two waveriders developed by means of Hypersonic Small Disturbance Theory for two elliptic cones are presented and analyzed for a wide range of Mach numbers and angles of attack. Various off-design performances of waverider with on-design performances are obtained and fully discussed. These data about aerodynamics and performaces of waveriders containing some important information for high speed flying objects could be used for the design of a hypersonic airplane which is being investigated as a future plane. Through entropy distributions for elliptic cones and vaveriders, the vortical layer which is quite difficult to be studied especially for a special body like a waverider is handled in this paper and numerical methods to catch the vortical layer more clearly are also discussed.

      더보기

      목차 (Table of Contents)

      • 1. INTRODUCTION
      • 2. AERODYNAMIC FORCE
      • 3. CIRCULAR- AND ELLIPTIC-CONE FLOW SOLUTIONS
      • 4. HYPERSONIC FLOW SOLUTION OF WAVERIDER
      • 5. CONCLUDING REMARK
      • 1. INTRODUCTION
      • 2. AERODYNAMIC FORCE
      • 3. CIRCULAR- AND ELLIPTIC-CONE FLOW SOLUTIONS
      • 4. HYPERSONIC FLOW SOLUTION OF WAVERIDER
      • 5. CONCLUDING REMARK
      더보기

      동일학술지(권/호) 다른 논문

      분석정보

      View

      상세정보조회

      0

      Usage

      원문다운로드

      0

      대출신청

      0

      복사신청

      0

      EDDS신청

      0

      동일 주제 내 활용도 TOP

      더보기

      주제

      연도별 연구동향

      연도별 활용동향

      연관논문

      연구자 네트워크맵

      공동연구자 (7)

      유사연구자 (20) 활용도상위20명

      이 자료와 함께 이용한 RISS 자료

      나만을 위한 추천자료

      해외이동버튼