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Computational Test Cases for a Clipped Delta Wing with Pitching and Trailing-Edge Control Surface Oscillations
| AUTHOR | Nasa, National Aeronautics and Space Adm |
| PUBLISHER | Independently Published (09/23/2018) |
| PRODUCT TYPE | Paperback (Paperback) |
Description
Computational test cases have been selected from the data set for a clipped delta wing with a six-percent-thick circular-arc airfoil section that was tested in the NASA Langley Transonic Dynamics Tunnel. The test cases include parametric variation of static angle of attack, pitching oscillation frequency, trailing-edge control surface oscillation frequency, and Mach numbers from subsonic to low supersonic values. Tables and plots of the measured pressures are presented for each case. This report provides an early release of test cases that have been proposed for a document that supplements the cases presented in AGARD Report 702.Bennett, Robert M. and Walker, Charlotte E.Langley Research CenterCOMPUTATIONAL FLUID DYNAMICS; DELTA WINGS; AIRFOIL PROFILES; CONTROL SURFACES; PITCH (INCLINATION); WIND TUNNEL TESTS; UNSTEADY AERODYNAMICS; TRANSONIC FLOW; COMPUTERIZED SIMULATION; ANGLE OF ATTACK; TRAILING EDGES; MACH NUMBER; WIND TUNNEL MODELS; ATTITUDE CONTROL; OSCILLATIONS...
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Product Format
Product Details
ISBN-13:
9781723946066
ISBN-10:
1723946060
Binding:
Paperback or Softback (Trade Paperback (Us))
Content Language:
English
More Product Details
Page Count:
92
Carton Quantity:
44
Product Dimensions:
8.50 x 0.19 x 11.02 inches
Weight:
0.52 pound(s)
Country of Origin:
US
Subject Information
BISAC Categories
Science | Space Science - General
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publisher marketing
Computational test cases have been selected from the data set for a clipped delta wing with a six-percent-thick circular-arc airfoil section that was tested in the NASA Langley Transonic Dynamics Tunnel. The test cases include parametric variation of static angle of attack, pitching oscillation frequency, trailing-edge control surface oscillation frequency, and Mach numbers from subsonic to low supersonic values. Tables and plots of the measured pressures are presented for each case. This report provides an early release of test cases that have been proposed for a document that supplements the cases presented in AGARD Report 702.Bennett, Robert M. and Walker, Charlotte E.Langley Research CenterCOMPUTATIONAL FLUID DYNAMICS; DELTA WINGS; AIRFOIL PROFILES; CONTROL SURFACES; PITCH (INCLINATION); WIND TUNNEL TESTS; UNSTEADY AERODYNAMICS; TRANSONIC FLOW; COMPUTERIZED SIMULATION; ANGLE OF ATTACK; TRAILING EDGES; MACH NUMBER; WIND TUNNEL MODELS; ATTITUDE CONTROL; OSCILLATIONS...
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