Blank Cover Image

Study of Potential Aerodynamic Benefits From Spanwise Blowing at Wingtip

Author(s):
Raymond E. Mineck  
Publication title:
NASA Technical Reports
Pub. Year:
1995
Issue:
NASA-TP-3515
Pt.:
NAS 1.60:3515
Paper no.:
N95-28669
Page(from):
1
Page(to):
102
Pages:
102
Pub. info.:
National Aeronautics and Space Adminstration
Language:
English
Type:
Technical Paper

Similar Items:

1 Technical Paper ASSENSMENT OF POTENTIAL AERODYNAMIC BENEFITS FROM SPANWISE BLOWING AT THE WING TIP

Mineck, Raymond Edward

National Aeronautics and Space Adminstration
7 Technical Paper WALL INTERFERENCE TESTS OF A CAST 10-2/DOA 2 AIRFOIL IN AN ADAPTIVE-WALL TEST SECTION

Mineck, Raymond E.

National Aeronautics and Space Administration
2 Technical Paper Flow Visualization Studies of Blowing From the Tip of a Swept Wing

Smith, Jannette W., Mineck, Raymond E., Neuhart, Dan H.

National Aeronautics and Space Adminstration
8 Technical Paper HARDWARE AND OPERATING FEATURES OF THE ADAPTIVE WALL TEST SECTION FOR THE 0.3-METER TRANSONIC CRYOGENIC TUNNEL

Mineck, Raymond E.

National Aeronautics and Space Administration
3 Technical Paper Aerodynamic Characteristics and Pressure Distributions for an Executive-Jet Baselin Airfoil Section

Allision, Dennis O., Mineck, Raymond E.

National Aeronautics and Space Adminstration
9 Technical Paper Wind-Tunnel Investigation of Aerodynamic Efficiency of Three Planar Elliptical Wings With Curvature of Quarter-Chord Line

Mineck, Raymond E., Vijgen, Paul M.H.W.

National Aeronautics and Space Adminstration
4 Technical Paper Effect of Full-Chord Porosity on Aerodynamic Characteristics of the NACA 0012 Airfoil

Raymond E. Mineck, Peter M. Hartwich

National Aeronautics and Space Adminstration
10 Technical Paper LOW-SPEED AERODYNAMIC CHARACTERISTICS OF A WING-CANARD CONFIGURATION WITH UNDERWING SPANWISE BLOWING ON THE

Banks, D. W.

National Aeronautics and Space Administration
5 Technical Paper A Study of the Potential Benefits Associated with the Development of a Dedicated Helicopter Transmission Lubricant

Drago,Raymond J., Mangione,Pasquale J., Wendrzycki,Raymond D.

"Society of Automotive Engineering, Inc."
11 Technical Paper Assessment of Dual-Point Drag Reduction for an Executive-Jet Modified Airfoil Section

Dennis O. Allison, Raymond E. Mineck

National Aeronautics and Space Adminstration
6 Technical Paper Comparison of a Two-Demensional Adaprive-Wall Technique With Analytical Wall Interferece Correction Techniques

Mineck, Raymond E.

National Aeronautics and Space Adminstration
12 Technical Paper Calibration of the 13- by 13-Inch Adaptive Wall Test Section for the Langley 0.3-Meter Transonic Cryogenic Tunnel

Mineck, Raymond E., Hill, Acquilla S.

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