Blank Cover Image

WIND TUNNEL RESULTS FOR A HIGH-SPEED, NATURAL LAMINAR-FLOW AIRFOIL DESIGNED FOR GENERAL AVIATION AIRCRAFT

著者名:
Sewall, William G. et al. ( NASA )  
掲載資料名:
NASA Technical Reports(N88-)
発行年:
1985
号:
NASA-TM-87602
通号:
G3/02 0117217
パート:
NAS1.15:87602
ペーパー番号:
N88-14078
開始ページ:
1
終了ページ:
73
総ページ数:
73
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:

1 テクニカルペーパー WIND-TUNNEL INVESTIGATION OF A FULL-SCALE GENERAL AVIATION AIRPLANE EQUIPPED WITH AN ADVANCED NATURAL LAMINAR FLOW WING

Murri, Daniel G. et al.

National Aeronautics and Space Administration
7 テクニカルペーパー General Aviation Aircraft Design Methodology in a PC Environment

Roskam, Jan, Anemaat, William A.

Society of Automotive Engineers
2 テクニカルペーパー A Wind Tunnel Study of Icing Effects on a Natural Laminar Flow Airfoil

Addy, Harold E., Jr., Chung, James J.

American Institute of Aeronautics and Astronautics
8 テクニカルペーパー Desigh of a Natural Laminar Flow Airfoil for an Unmanned Aircraft

SRILATHA, K R, PAMAMOORTHY, P

National Aeronautics and Space Adminstration
3 テクニカルペーパー Simulation of Vortex Wake Impact on a General-Aviation Aircraft Model in a Wind Tunnel Using the Airfoil Lattice

Mikhailov, Yu.S.

Society of Automotive Engineers
9 テクニカルペーパー EXPERIMENTAL RESULTS FOR A FLAPPED NATURAL-LAMINAR-FLOW AIRFOIL WITH HIGH LIFT DRAG RATIO

McGhee, R.J.

National Aeronautics and Space Administration
4 テクニカルペーパー An Experimental Study of a General Aviation Single-Engine Aircraft Utilizing a Natural Laminar Flow Wing

Ostowari,C., Naik,D.A.

"Society of Automotive Engineering, Inc."
10 テクニカルペーパー A method for the constrained design of natural laminar flow airfoils

Green, Bradford E., Whitesider, John L., Campbell, Richard L., Mineck, Raymond E.

American Institute of Aeronautics and Astronautics
5 テクニカルペーパー FLIGHT TEST INVESTIGATION OF CERTIFICATION ISSUES PERTAINING TO GENERAL-AVIATION-TYPE AIRCRAFT WITH NATURAL LAMINAR FLOW

DOTY, WAYNE A.

National Aeronautics and Space Adminstration
11 テクニカルペーパー An Approach to the Constrained Design of Natural Laminar Flow Airfoils

Green, Bradford E.

National Aeronautics and Space Adminstration
6 テクニカルペーパー The Next Generation of High-Speed Dynamic Stability Wind Tunnel Testing (Invited)

D. Tomek, W. Sewall, S. Mason, B. Szchur

American Institute of Aeronautics and Astronautics
12 テクニカルペーパー An approach to the constrained design of natural laminar flow airfoils

Green, Bradford Earl

National Aeronautics and Space Adminstration
1
 
2
 
3
 
4
 
5
 
6
 
7
 
8
 
9
 
10
 
11
 
12