首页
学术期刊
论文检测
AIGC检测
热点
更多
数据
UNSTEADY TRANSONIC THIN-AIRFOIL THEORY FOR POWER-LAW UPWASH.
被引:0
|
作者
:
Plotkin, A.
论文数:
0
引用数:
0
h-index:
0
Plotkin, A.
机构
:
来源
:
Journal of Applied Mechanics, Transactions ASME
|
1978年
/ 45卷
/ 02期
关键词
:
D O I
:
暂无
中图分类号
:
学科分类号
:
摘要
:
引用
收藏
页码:440 / 441
相关论文
共 50 条
[1]
UNSTEADY TRANSONIC THIN-AIRFOIL THEORY FOR POWER-LAW UPWASH
PLOTKIN, A
论文数:
0
引用数:
0
h-index:
0
机构:
UNIV MARYLAND,INST PHYS SCI,COLLEGE PK,MD 20742
UNIV MARYLAND,INST PHYS SCI,COLLEGE PK,MD 20742
PLOTKIN, A
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME,
1978,
45
(02):
: 440
-
441
[2]
LIFT AND MOMENT FOR ARBITRARY POWER-LAW UPWASH IN OSCILLATING SUBSONIC UNSTEADY THIN-AIRFOIL THEORY
KEMP, NH
论文数:
0
引用数:
0
h-index:
0
机构:
AVCO EVERETT RES LAB INC,EVERETT,MA 02149
AVCO EVERETT RES LAB INC,EVERETT,MA 02149
KEMP, NH
AIAA JOURNAL,
1974,
12
(03)
: 413
-
415
[3]
UNSTEADY THIN-AIRFOIL THEORY FOR SUBSONIC FLOW
OSBORNE, C
论文数:
0
引用数:
0
h-index:
0
机构:
CORNELL UNIV,ITHACA,NY 14850
CORNELL UNIV,ITHACA,NY 14850
OSBORNE, C
AIAA JOURNAL,
1973,
11
(02)
: 205
-
209
[4]
COMPRESSIBILITY EFFECTS IN UNSTEADY THIN-AIRFOIL THEORY
AMIET, RK
论文数:
0
引用数:
0
h-index:
0
机构:
UNITED AIRCRAFT RES LABS,E HARTFORD,CT 06108
UNITED AIRCRAFT RES LABS,E HARTFORD,CT 06108
AMIET, RK
AIAA JOURNAL,
1974,
12
(02)
: 252
-
255
[5]
APPROXIMATE UNSTEADY THIN-AIRFOIL THEORY FOR SUBSONIC FLOW
KEMP, NH
论文数:
0
引用数:
0
h-index:
0
机构:
AVCO CORP,EVERETT RES LAB,EVERETT,MA 02149
KEMP, NH
HOMICZ, G
论文数:
0
引用数:
0
h-index:
0
机构:
AVCO CORP,EVERETT RES LAB,EVERETT,MA 02149
HOMICZ, G
AIAA JOURNAL,
1976,
14
(08)
: 1083
-
1089
[6]
IMPROVED THIN-AIRFOIL THEORY
ZEDAN, MF
论文数:
0
引用数:
0
h-index:
0
机构:
King Saud Univ, Saudi Arabia
ZEDAN, MF
ABUABDOU, K
论文数:
0
引用数:
0
h-index:
0
机构:
King Saud Univ, Saudi Arabia
ABUABDOU, K
JOURNAL OF AIRCRAFT,
1988,
25
(12):
: 1122
-
1128
[7]
Unsteady Thin-Airfoil Theory Revisited: Application of a Simple Lift Formula
Liu, Tianshu
论文数:
0
引用数:
0
h-index:
0
机构:
Western Michigan Univ, Dept Mech & Aerosp Engn, Kalamazoo, MI 49008 USA
Western Michigan Univ, Dept Mech & Aerosp Engn, Kalamazoo, MI 49008 USA
Liu, Tianshu
Wang, Shizhao
论文数:
0
引用数:
0
h-index:
0
机构:
Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China
Western Michigan Univ, Dept Mech & Aerosp Engn, Kalamazoo, MI 49008 USA
Wang, Shizhao
Zhang, Xing
论文数:
0
引用数:
0
h-index:
0
机构:
Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China
Western Michigan Univ, Dept Mech & Aerosp Engn, Kalamazoo, MI 49008 USA
Zhang, Xing
He, Guowei
论文数:
0
引用数:
0
h-index:
0
机构:
Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China
Western Michigan Univ, Dept Mech & Aerosp Engn, Kalamazoo, MI 49008 USA
He, Guowei
AIAA JOURNAL,
2015,
53
(06)
: 1492
-
1502
[8]
CLOSED-FORM LIFT AND MOMENT FOR OSBORNES UNSTEADY THIN-AIRFOIL THEORY
KEMP, NH
论文数:
0
引用数:
0
h-index:
0
机构:
AVCO EVERETT RES LAB INC,EVERETT,MA 02149
AVCO EVERETT RES LAB INC,EVERETT,MA 02149
KEMP, NH
AIAA JOURNAL,
1973,
11
(09)
: 1358
-
1360
[9]
IMPROVED THIN-AIRFOIL THEORY - REPLY
ZEDAN, MF
论文数:
0
引用数:
0
h-index:
0
ZEDAN, MF
ABUABDOU, K
论文数:
0
引用数:
0
h-index:
0
ABUABDOU, K
JOURNAL OF AIRCRAFT,
1990,
27
(05):
: 479
-
480
[10]
IMPROVED THIN-AIRFOIL THEORY - COMMENT
PLOTKIN, A
论文数:
0
引用数:
0
h-index:
0
机构:
San Diego State University, San Diegos, CA
PLOTKIN, A
JOURNAL OF AIRCRAFT,
1990,
27
(05):
: 478
-
479
←
1
2
3
4
5
→