Muutke küpsiste eelistusi

Assessment of Wingtip Modifications to Increase the Fuel Efficiency of Air Force Aircraft [Pehme köide]

  • Formaat: Paperback / softback, 112 pages, kõrgus x laius: 229x152 mm
  • Ilmumisaeg: 06-Sep-2007
  • Kirjastus: National Academies Press
  • ISBN-10: 0309104971
  • ISBN-13: 9780309104975
Teised raamatud teemal:
  • Formaat: Paperback / softback, 112 pages, kõrgus x laius: 229x152 mm
  • Ilmumisaeg: 06-Sep-2007
  • Kirjastus: National Academies Press
  • ISBN-10: 0309104971
  • ISBN-13: 9780309104975
Teised raamatud teemal:
The high cost of aviation fuel has resulted in increased attention by Congress and the Air Force on improving military aircraft fuel efficiency. One action considered is modification of the aircrafta (TM)s wingtip by installing, for example, winglets to reduce drag. While common on commercial aircraft, such modifications have been less so on military aircraft. In an attempt to encourage greater Air Force use in this area, Congress, in H. Rept. 109-452, directed the Air Force to provide a report examining the feasibility of modifying its aircraft with winglets. To assist in this effort, the Air Force asked the NRC to evaluate its aircraft inventory and identify those aircraft that may be good candidates for winglet modifications. This reporta "which considers other wingtip modifications in addition to wingletsa "presents a review of wingtip modifications; an examination of previous analyses and experience with such modifications; and an assessment of wingtip modifications for various Air Force aircraft and potential investment strategies.
Summary 1(11)
Background and Overview
12(6)
Introduction
12(3)
Statement of Task
15(1)
Scope and Committee Approach
15(2)
Structure of This Report
17(1)
Wingtip Modifications
18(13)
History of Wingtip Devices
18(1)
Introduction to Wingtip Aerodynamics
19(3)
Design of Wingtip Devices
22(3)
Optimal Wingspan
22(1)
Wing Retrofits
23(2)
Benefits of Wingtip Modifications
25(2)
Reduced Fuel Burn
25(1)
Increased Payload-Range Capability
25(2)
Improved Takeoff Performance
27(1)
Challenges Associated with Wingtip Modifications
27(2)
Cost
27(1)
Added Weight
28(1)
Added Span and Height
28(1)
Interference with Other Wing Equipment
29(1)
General Observations
29(2)
Previous Analyses and Experience with Wingtip Modifications on Existing Aircraft
31(22)
Early Research Programs
31(1)
NASA Led Research: ACEE
31(1)
Commerical Experience
32(16)
Airframe Manufactures
33(10)
Airlines
43(5)
Military Experience
48(3)
C-17
48(2)
C-32
50(1)
KC-135
50(1)
Summary of Commercial and Military Experience
51(2)
Assessment of Wingtip Modifications for Various Air Force Aircraft and Potential Investment Strategies
53(37)
Checklist for Making Wingtip Modification Decisions
53(4)
Technical Issues
54(1)
Economic Issues
55(1)
Putting It All Together
56(1)
Candidate Aircraft in the Air Force Inventory
57(6)
C-17
58(1)
KC-135R/T
58(1)
C-5
59(1)
KC-10
59(1)
C-130H/J
60(1)
Intelligence, Surveillance, and Reconnaissance Aircraft
61(1)
Other Air Force Aircraft
61(2)
Priority Aircraft to Be Considered for Wingtip Modification
63(1)
Preliminary Net Present Value Analysis
63(6)
Investment Strategies
69(6)
Performing Retrofit Studies and Implementing Modifications
70(2)
Financing Mechanisms
72(3)
APPENDIXES
Data Used in Net Present Value Analyses
75(2)
Additional Methods for Improving Fuel Consumption
77(11)
Presentations to the Committee
88(2)
Biographical Sketches of Committee Members
90


Committee on Assessment of Aircraft Winglets for Large Aircraft Fuel Efficiency, National Research Council