EVALUATION AND IMPROVEMENT OF LIQUID PROPELLANT ROCKET CHUGGING ANALYSIS TECHNIQUES. PART 2: A STUDY OF LOW FREQUENCY COMBUSTION INSTABILITY IN ROCKET ENGINE PREBURNERS USING A HETEROGENEOUS
- 著者名:
- Bartrand, Timothy A. ( Tennessee Univ. )
- 掲載資料名:
- NASA Technical Reports(N88-)
- 発行年:
- 1988
- 号:
- NASA-CR-182724
- 通号:
- G3/20 0154092
- パート:
- NAS1.26:182724
- ペーパー番号:
- N88-27225
- 開始ページ:
- 1
- 終了ページ:
- 229
- 総ページ数:
- 229
- 出版情報:
- National Aeronautics and Space Administration
- 言語:
- 英語
- 資料種別:
- テクニカルペーパー
類似資料:
National Aeronautics and Space Administration |
7
テクニカルペーパー
Simulation of spray combustion instabilities in liquid rocket engines, part 1: methodology
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
5
テクニカルペーパー
Performance of a supercharged direct-injection stratified-charge rotary combustion engine
National Aeronautics and Space Adminstration |
"Society of Automotive Engineering, Inc." |
6
テクニカルペーパー
Simulation of spray combustion instabilities in liquid rocket engines, part II: applications
American Institute of Aeronautics and Astronautics |
12
テクニカルペーパー
Obserbation of Lox/Hydrogen Combustion Flame in a Rocket Chamber During Chugging Instability
American Institute of Aeronautics and Astronautics |