THE 0.6 M X 0.6 M TRISONIC TEST SECTION (TMK) OF DFVLR IN COLOGNE-PORZ (STATUS 1986)
- Author(s):
- ESCH, H. ( ESA, PARIS )
- Publication title:
- NASA Technical Reports(N88-)
- Pub. Year:
- 1987
- Issue:
- ESA-TT-1052
- Paper no.:
- N88-11681
- Page(from):
- 1
- Page(to):
- 89
- Pages:
- 89
- Pub. info.:
- National Aeronautics and Space Administration
- Language:
- English
- Type:
- Technical Paper
Similar Items:
National Aeronautics and Space Administration |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Administration |
8
Technical Paper
SUPERSONIC WALL ADAPTATION IN THE RUBBER TUBE TEST SECTION OF THE DFVLR GOETTINGEN
National Aeronautics and Space Administration |
National Aeronautics and Space Administration |
9
Technical Paper
Flow Characteristics Around a Tapered Circular Cylinder Within Mach Number Range 0.6-1.2
American Institute of Aeronautics and Astronautics |
4
Technical Paper
AERODYNAMICS OF A SPHERE AND AN OBLATE SPHEROID FOR MACH NUMBERS FROM 0.6 TO 10.5 INCLUDING SOME EFFECTS OF TEST CONDITIONS
National Aeronautics and Space Adminstration |
10
Technical Paper
Experimental Investigation of the Pressure-Velocity Correlation of a M=0.6 Axisymmetric Jet
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Administration |
National Aeronautics and Space Adminstration |
National Aeronautics and Space Administration |
Society of Automotive Engineers |