scholarly journals F-14 Inlet Development Experience

1982 ◽  
Author(s):  
R. H. Tindell ◽  
C. A. Hoelzer ◽  
D. Alexander
Keyword(s):  
Wind Tunnel ◽  
Flight Test ◽  
Test Results ◽  
Development Experience ◽  
F 14

This paper reviews the F-14 inlet design and discusses the wind tunnel and flight test results of investigations that can contribute to more advanced inlet designs.

F-14 Inlet Development Experience

1982 ◽  
Vol 104 (4) ◽  
pp. 751-759
Author(s):  
R. H. Tindell ◽  
C. A. Hoelzer ◽  
D. Alexander
Keyword(s):  
Wind Tunnel ◽  
Flight Test ◽  
Test Results ◽  
Development Experience ◽  
F 14

This paper reviews the F-14 inlet design and discusses the wind tunnel and flight test results of investigation that can contribute to move advanced inlet design.

scholarly journals F-14 Re-Engining With the F110 Engine

1985 ◽  
Author(s):  
O. T. Castells ◽  
J. T. Strong
Keyword(s):  
Flight Test ◽  
Test Results ◽  
Design Features ◽  
Engine Design ◽  
Engine Development ◽  
F 14

The advantages of re-engining the F-14 aircraft with the F110 engine is presented. The areas of improvement and the engine development philosophy are explained. A summary description of the pertinent engine design features of the F110 are presented. The flight test results on inlet/engine compatability, afterburner operation, airplane performance, and maintainability/reliability/durability are interpreted. Finally, a description of the proposed version of the F110 engine for the F-14 is presented.

Analysis of the correlation of wind tunnel and ground test data to flight test results

1965 ◽  
Author(s):  
A. NAGEL ◽  
A. THOMAS
Keyword(s):  
Wind Tunnel ◽  
Test Data ◽  
Flight Test ◽  
Test Results ◽  
Ground Test

Using Wind Tunnel Tests for Slung-Load Clearance, Part 2: Other Loads

2014 ◽  
Vol 59 (4) ◽  
pp. 1-12
Author(s):  
Reuben Raz ◽  
Aviv Rosen ◽  
Luigi S. Cicolani ◽  
Jeffery Lusardi ◽  
Bryan Gassaway ◽  
...  
Keyword(s):  
Wind Tunnel ◽  
Flight Test ◽  
Test Results ◽  
Wind Tunnel Tests ◽  
Reduce Risk ◽  
Good Agreement

The first new load is the TRIO container that can be flown in three configurations with different heights. The second new load is a ribbon bridge interior bay section. Wind tunnel results with models of the new loads exhibit in general good agreement with flight-test results. The results of the new loads strengthen further the approach of using wind tunnel tests to accelerate slung-load clearance, as well as reduce risk and cost.

CORRELATION OF WIND TUNNEL AND FLIGHT TEST RESULTS

1940 ◽  
Author(s):  
W. W. Symington
Keyword(s):  
Wind Tunnel ◽  
Flight Test ◽  
Test Results

F/A-18C/JDAM CFD challenge wind tunnel and flight test results

1999 ◽  
Author(s):  
A. Cenko
Keyword(s):  
Wind Tunnel ◽  
Flight Test ◽  
Test Results

Cloud Phase Discrimination Using the Optical Icing Conditions Detector: Wind Tunnel and Flight Test Results

2011 ◽  
Author(s):  
Kaare J. Anderson ◽  
Gary E. Halama ◽  
Mark D. Ray ◽  
Michael P. Nesnidal ◽  
Robert Ide ◽  
...  
Keyword(s):  
Wind Tunnel ◽  
Flight Test ◽  
Test Results ◽  
Phase Discrimination

Flight test results for a high-capacity single-groove heat pipe

1992 ◽  
Author(s):  
J. AMBROSE ◽  
H. HOLMES ◽  
R. CIMA ◽  
M. KAPOLNEK
Keyword(s):  
Heat Pipe ◽  
High Capacity ◽  
Flight Test ◽  
Test Results
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