Environmental Assessment of Short-Term Construction Projects at the 150th Fighter Wing, New Mexico Air National Guard, Kirtland Air Force Base, New Mexico

2003 ◽  
Author(s):  
URS CORP OAKLAND CA
Keyword(s):  
New Mexico ◽  
Air Force ◽  
Environmental Assessment ◽  
Construction Projects ◽  
National Guard ◽  
Short Term ◽  
Air National Guard ◽  
Air Force Base

Programmatic Environmental Assessment (EA) for Minor Construction Projects at F. E. Warren Air Force Base, Wyoming

2013 ◽  
Author(s):  
Travis Beckwith ◽  
LiJane Brunner ◽  
Andy McKinley ◽  
Kurt Warmbier ◽  
Shain Wright
Keyword(s):  
Air Force ◽  
Environmental Assessment ◽  
Construction Projects ◽  
Air Force Base

Environmental Assessment: Recapitalization of the 49th WG Combat Capabilities and Capacities, Holloman Air Force Base, New Mexico

2011 ◽  
Author(s):  
Jr. Austin ◽  
Barringer John K. ◽  
Baxter Debra S. ◽  
Crabtree Rachel D. ◽  
Dehn Chris ◽  
...  
Keyword(s):  
New Mexico ◽  
Air Force ◽  
Environmental Assessment ◽  
Air Force Base

Final Environmental Assessment for San Andres Water Line, Holloman Air Force Base, Otero County, New Mexico

2007 ◽  
Author(s):  
Roger Berry ◽  
Jonathan Damp ◽  
Jeanne Dye ◽  
Jace Fahnestock ◽  
Rusty Gilbert ◽  
...  
Keyword(s):  
New Mexico ◽  
Air Force ◽  
Environmental Assessment ◽  
Water Line ◽  
Air Force Base ◽  
San Andres

Antonomous Environmental Definition of C-130 Flap Well Skin Panel

2005 ◽  
Vol 48 (1) ◽  
pp. 50-61 ◽  
Author(s):  
David Banaszak ◽  
Dansen Brown ◽  
David Laird
Keyword(s):  
North Carolina ◽  
Air Force ◽  
Engine Speed ◽  
National Guard ◽  
Air National Guard ◽  
Repair Patch ◽  
Right Hand ◽  
Time Histories ◽  
Air Force Base ◽  
The Right

Air Force C-130 aircraft require numerous aluminum doubler repairs on the wing flap skin aft of the right-hand outboard engine. These repairs are costly and require riveting. Rivets often provide new areas of stress concentration, which causes new cracks to develop elsewhere. Boeing and the Air Force Research Laboratory (AFRL) are measuring the thermal and strain environment behind the right-hand outboard engine of a North Carolina Air National Guard (NCANG) operational C-130 aircraft (TN 93-1456) for use in design of a damped repair patch to prevent the growth of cracks in skin under the wing flap panel. During June 2003. AFRL engineers and technicians acquired data using an autonomous damage dosimeter during five operational C-130 flights. The damage dosimeter measures structural strains and temperatures on in-service aircraft to diagnose structural conditions that are difficult to analyze, such as acoustics and high cycle fatigue (HCF). The first flight was from Charlotte, North Carolina to Warner Robins Air Force Base (AFB), Georgia and returned to Charlotte. The last four flights were assault flights where the C-130 simulated cargo drops. Pilots logged the altitude and indicated airspeed, engine speed, and flap positions for the first four flights. Flap position settings were compared with dosimeter temperature and root mean square (rms) strain measurements. This paper presents typical third octave plots showing engine speed vibratory frequencies, rms time histories (TH), and correlation data for a flight. This paper also presents typical limited data in TH, probability density function (PDF), power spectral density (PSD), and rain flow formats.

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