|
Aerodynamics
Anon.: Advanced Technology Airfoil Research,
Vol. II. NASA CP-2046, 1979.
Anon.: Supercritical Wing Technology—A
Report on Flight Evaluations. NASA SP-301,
1972.
Ethell, Jeffrey L.: Fuel
Economy in Aviation. NASA SP-462, 1983.
Flechner, Stuart G.; and
Jacobs, Peter F.: Experimental Results of Winglets
on First, Second, and Third Generation Jet Transports.
CTOL Transport Technology—1978. NASA
CP-2036, Pt. 1, 1978, pp. 553–569.
Flechner, Stuart G.; and
Jacobs, Peter F.: Experimental Results of Winglets
on First, Second, and Third Generation Jet Transports.
NASA TM-72674, 1978.
Hallion, Richard P.: On
the Frontier—Flight Research at Dryden,
1946–1981. NASA SP-4303, 1984.
Harris, Charles D.: NASA
Supercritical Airfoils—A Matrix of Family-Related
Airfoils. NASA TP-2969, 1990.
Hodge, Kenneth E.: Proceedings
of the F-8 Digital Fly-by-Wire and Supercritical
Wing First Flight’s 20th Anniversary Celebration.
NASA CP-3256, Vols. I and II, 1996.
Holmes, Bruce J.: Flight
Evaluation of an Advanced Technology Light Twin-Engine
Airplane (ATLIT). NASA CR-2832, 1977.
Kutney, John T.; and Piszkin,
Stanley P.: Reduction of Drag Rise of the Convair
990 Airplane. J. Aircr., vol. 1, no. 1,
Jan.–Feb. 1964, pp. 8–12. (Also available
as AIAA Paper 63-276.)
Langhans, Richard A.; and
Flechner, Stuart G.: Wind-Tunnel Investigation
at Mach Numbers From 0.25 to 1.01 of a Transport
Configuration Designed to Cruise at Near-Sonic
Speeds. NASA TM X-2622, 1972.
Lin, J. C.: Control of Turbulent Boundary-Layer
Separation Using Micro-Vortex Generators. AIAA
Paper 99-3404, 1999.
Lynch, F. T.: Commercial
Transports—Aerodynamic Design for Cruise
Performance Efficiency. Progress in Astronautics
and Aeronautics, D. Nixon, ed., Vol. 81, AIAA,
1982, pp. 81–147.
McGhee, Robert J.; and
Beasley, William D.: Low-Speed Aerodynamic Characteristics
of a 17-Percent-Thick Airfoil Section Designed
for General Aviation Applications. NASA TN
D-7428, 1973.
Porter, Donald J.: The
Cessna Citations. TAB Books, 1993.
Potsdam, M. A.; Intemann, G. A.; Frink, N. T.;
Campbell, R. L.; and Smith, L. A.: Wing/Pylon Fillet
Design Using Unstructured Mesh Euler Solvers. AIAA
Paper 93-3500, 1993.
Reynolds, P. T.; Gertsen, W. M.; and Voorhees,
C. G.: Gates Learjet Model 28/29, the First “Longhorn”
Learjet. AIAA Paper 78-1445, 1978.
Somers, Dan M.: Subsonic
Natural-Laminar-Flow Airfoils. Natural Laminar
Flow and Laminar Flow Control, R. W. Barnwell
and M. Y. Hussaini, eds., Springer-Verlag, 1992,
pp. 143–176.
Somers, Dan M.: Design
and Experimental Results for a Natural-Laminar-Flow
Airfoil for General Aviation Application. NASA
TP-1861, 1981.
Staff, Douglas Aircraft
Co.: DC-10 Winglet Flight Evaluation. NASA
CR-3704, 1983.
Szurovy, Geza: Learjets. Motorbooks International.
1996.
Whitcomb, Richard T.: Interview with Author, August
16, 2000. (Unpublished)
Whitcomb, Richard T.: Research on Methods for Reducing
the Aerodynamic Drag at Transonic Speeds. The Inaugural
ICASE/LaRC Eastman Jacobs Lecture presented at
the Langley Research Center, November 14, 1994.
(Unpublished)
Whitcomb, Richard T.: A
Design Approach and Selected Wind-Tunnel Results
at High Subsonic Speeds for Wing-Tip Mounted Winglets.
NASA TN D-8260, 1976.
Whitcomb, Richard T.; and
Sevier, John R., Jr.: A Supersonic Area Rule
and an Application to the Design of a Wing-Body
Combination With High Lift-Drag Ratios. NASA
TR R-72, 1960. (Supersedes NACA RM L53H31a.)
Whitcomb, Richard T.: A
Fuselage Addition To Increase Drag-Rise Mach Number
of Subsonic Airplanes at Lifting Conditions.
NACA TN 4290, 1958.
Whitcomb, Richard T.:
Special Bodies Added on a Wing To Reduce Shock-Induced
Boundary-Layer Separation at High Subsonic Speeds.
NACA TN 4293, 1958.
Whitcomb, Richard T.: A
Study of the Zero-Lift Drag-Rise Characteristics
of Wing-Body Combinations Near the Speed of Sound.
NACA Rep. 1273, 1956. (Supersedes NACA RM L52H08.)
Williams, B.: Advanced Technology Transport Configuration
Development. AIAA Paper 72-756, Aug. 1972.
Aeroelasticity
Abbott, Frank T., Jr.; Kelly,
H. Neale; and Hampton, Kenneth D.: Investigation
of Propeller-Power-Plant Autoprecession Boundaries
for a Dynamic-Aeroelastic Model of a Four-Engine
Turboprop Transport Airplane. NASA TN D-1806,
1963.
Bahatia, K. G.; Nagaraja, K. S.; and Ruhlin, C.
L.: Winglet Effects on the Flutter of Twin-Engine-Transport
Type Wing. AIAA Paper 84-0905, 1984.
Bennett, Robert M.; Kelly,
H. Neale; and Gurley, John D.: Investigation
of 1/8-Size Dynamic-Aeroelastic Model of the Lockheed
Electra Airplane in the Langley Transonic Dynamics
Tunnel. NASA TM SX-456, FAA, 1960.
Bland, Samuel R.; and Bennett,
Robert M.: Wind-Tunnel Measurement of Propeller
Whirl-Flutter Speeds and Static-Stability Derivatives
and Comparison With Theory. NASA TN D-1807,
1963.
Cole, Stanley R.; and Garcia, Jerry L.: Past, Present,
and Future Capabilities of the Transonic Dynamics
Tunnel From an Aeroelasticity Perspective. AIAA
Paper 2000-1767, 2000.
Corliss, James M.; and Cole, Stanley R.: Heavy
Gas Conversion of the NASA Langley Transonic Dynamics
Tunnel. AIAA Paper 98-2710, June 1998.
Doggett, Robert V., Jr.;
and Farmer, Moses G.: Preliminary Study of Effects
of Winglets on Wing Flutter. NASA TM X-3433,
1976.
Farmer, M. G.: Flutter
Studies To Determine Nacelle Aerodynamic Effects
on a Fan-Jet Transport Model for Two Mount Systems
and Two Wind Tunnels. NASA TN D-6003, 1970.
Farmer, Moses G.; and Florance,
James R.: Boeing 777 Flutter Model Test Conducted
in TDT. Research and Technology Highlights—1993.
NASA TM-4575, 1993, pp. 25–26.
Garrison, Peter: The Hammer.
Air & Space Magazine, Feb./Mar. 2001.
Keller, Donald F.: Flutter
Study of Simple Business-Jet Wing Conducted in
TDT. Research and Technology Highlights—1993.
NASA TM-4575, 1993, p. 19.
Rauch, Frank J.; and Clark, William B.: Results
of Test Conducted on Gulfstream G-V Wing Conducted
on a 1/10th Scale Flutter Model. Rep. GV-GER-614,
Gulfstream Aerospace, Mar. 1993.
Reed, Wilmer H., III; and
Bland, Samuel R.: An Analytical Treatment of
Aircraft Propeller Precession Instability.
NASA TN D-659, 1961.
Ricketts, Rodney H.: Experimental
Aeroelasticity—History, Status and Future
in Brief. NASA TM-102651, 1990. (Also available
as AIAA Paper 90-0978.)
Rivera, Jose A., Jr.; and Florance, James R.: Contributions
of Transonic Dynamics Tunnel Testing to Airplane
Flutter Clearance. AIAA Paper 2000-1768, 2000.
Ruhlin, C. L.; Rauch, F.
J.; and Waters, C.: Transport Flutter Study
of a Wind Tunnel Model of a Supercritical Wing
With/Without Winglet. NASA TM-83279, 1982.
Flight Dynamics
Bennett, George: Flight
Test of a Stall Sensor and Evaluation of Its Application
to an Aircraft Stall Deterrent System Using the
NASA RC General Aviation Simulator. NASA CR-146324,
1976.
Bowman, James S., Jr.:
Summary of Spin Technology as Related to Light
General-Aviation Airplanes. NASA TN D-6575,
1971.
Chambers, Joseph R.; and Stough, H. Paul, III:
Summary of NASA Stall/Spin Research for General
Aviation Configurations. AIAA Paper 86-2597, 1986.
Chevalier, Howard L.: Summary
of Theoretical Considerations and Wind-Tunnel Tests
of an Aerodynamic Spoiler for Stall Proofing a
General Aviation Airplane. NASA CR-165100,
1982.
Feistel, T. W.; Anderson, S. B.; and Kroeger, R.
A.: A Method for Localizing Wing Flow Separation
at Stall To Alleviate Spin Entry Tendencies. AIAA
Paper 78-1476, 1978.
Fink, Marvin P.; and Freeman,
Delma C., Jr.: Full-Scale Wind-Tunnel Investigation
of Static Longitudinal and Lateral Characteristics
of a Light Twin-Engine Airplane. NASA TN D-4983,
1969.
Holcomb, M. L.: The Beach Model 77 “Skipper”
Spin Program. AIAA Paper 79-1835, 1979.
Holcomb, M. L.; and Tumlinson, R. R.: Evaluation
of a Radio-Control Model for Spin Simulation. SAE
Paper 770482, 1977.
Lina, L. J.; and Moul, M. T.: A Simulator Study
of T-Tail Aircraft in Deep Stall Conditions. AIAA
Paper 65-781, 1965.
Montgomery, R. C.; and Moul, M. T.: Analysis of
Deep-Stall Characteristics of T-Tailed Aircraft
Configurations and Some Recovery Procedures. AIAA
Paper 66-13, 1966.
Ray, E. J.; and Taylor, R. T.: A Systematic Study
of the Factors Contributing to Post-Stall Longitudinal
Stability of T-Tail Transport Configurations. AIAA
Paper 65-737, 1965.
Satran, Dale R.: Wind-Tunnel
Investigation of the Flight Characteristics of
a Canard General-Aviation Airplane Configuration.
NASA TP-2623, 1986.
Shevell, Richard S.; and Schaufele, Roger D.: Aerodynamic
Design Features of the DC-9. J. Aircr., vol. 3,
no. 6, Nov.–Dec. 1966, pp. 515–523.
(Also available as AIAA Paper No. 65-738).
Staff of Langley Research
Center: Exploratory Study of the Effects of
Wing-Leading-Edge Modifications on the Stall/Spin
Behavior of a Light General Aviation Airplane.
NASA TP-1589, 1979.
Stough, H. Paul; and DiCarlo, Daniel J.: Spin Resistance
Development for Small Airplanes—A Retrospective.
SAE Paper 2000-01-1691, 2000.
Stough, H. Paul, III; DiCarlo, Daniel J.; and Patton,
James M., Jr.: Evaluation of Airplane Spin Resistance
Using Proposed Criteria for Light General Aviation
Airplanes. AIAA Paper 87-2562-CP, 1987.
Taylor, Robert T.; and
Ray, Edward J.: Deep-Stall Aerodynamic Characteristics
of T-Tail Aircraft. Conference on Aircraft Operating
Problems. NASA SP-83, 1965, pp. 113–121.
Yip, L. P.: Wind-Tunnel
Investigation of a Full-Scale Canard-Configured
General Aviation Airplane. NASA TP-2382, 1985.
Yip, Long P.; Ross, Holly
M.; and Robelen, Donald B.: Model Flight Tests
of a Spin-Resistant Trainer Configuration. J.
Aircr., vol. 29, no. 5, Sept.–Oct. 1992,
pp. 799–805.
Operating Problems
Anon.: Safety Issues Related
to Wake Vortex Encounters During Visual Approach
to Landing. Flight Safety Digest, Flight
Safety Foundation, June 1994.
Anon.: Wake Vortex Minimization.
NASA SP-409, 1976.
Arbuckle, P. D.; Lewis,
M. S.; and Hinton, D. A.: Airborne Systems Technology
Application to the Windshear Threat. 20th Congress
of the International Council of the Aeronautical
Sciences, 1996, pp. 1640–1650. (Also
available as ICAS paper 96-5.7.1.)
Bowles, Roland L.: Windshear
Detection and Avoidance—Airborne Systems
Survey. Proceedings of the 29th IEEE Conference
on Decision and Control, Vol. 2, 1990, pp.708–736.
Brandon, Jay M.; Jordan,
Frank L., Jr.; Buttrill, Catherine W.; and Stuever,
Robert A.: Application of Wind Tunnel Free-Flight
Technique for Wake Vortex Encounters. NASA
TP-3672, 1997.
Caracena, Fernando; Holle,
Ronald L.; and Doswell, Charles A., III: Microbursts—A
Handbook for Visual Identification. National
Severe Storms Lab., 1990.
Carden, Huey D.: Evaluation
of Emergency-Locator-Transmitter Performance in
Real and Simulated Crash Tests. NASA TM-81960,
1981.
Carden, Huey D.; and Hayduk, Robert J.: Aircraft
Subfloor Response to Crash Loadings. SAE Paper
810614, Apr. 1981.
Dunham, R. E., Jr.; Stuever, Robert A.; and Vicroy,
Dan D.: The Challenges of Simulating Wake Vortex
Encounters and Assessing Separation Criteria. AIAA
Paper 93-3568, 1993.
Fasanella, Edwin L.; Widmayer,
E.; and Robinson, Martha P.: Structural Analysis
of the Controlled Impact Demonstration of a Jet
Transport Airplane. J. Aircr., vol. 24,
no. 4, Apr. 1987, pp. 274–280.
Fisher, Bruce D.: Effects of Lightning on Operations
of Aerospace Vehicles. Presented at the AGARD Flight
Mechanics Panel Symposium on Flight in Adverse
Environmental Conditions (Gol, Norway). May 8–11,
1989, paper 20.
Fisher, Bruce D.; and Plumer,
J. Anderson: Managing Risk From Lightning Strikes
to Aircraft. Human Factors and Risk Management
in Advanced Technology: 40th Annual International
Air Safety Seminar Proceedings, Flight Safety
Foundation, 1987, pp. 353–375.
Fisher, Lloyd J.: Factors
Affecting Ditching of New Transport Airplanes.
NASA Aircraft Safety and Operating Problems,
Vol. 1, NASA SP-270, 1971, pp. 1–10.
Hastings, Earl C., Jr.;
Shanks, Robert E.; Champine, Robert A.; Copeland,
W. Latham; and Young, Douglas C.: Preliminary
Results of Flight Tests of Vortex Attenuating Splines.
NASA TM X-71928, 1974.
Hinton, D. A.: An Aircraft Vortex Spacing System
(AVOSS) for Dynamical Wake Vortex Spacing Criteria.
Presented at 78th Fluid Dynamics Panel Symposium
(Trondheim, Norway), May 20–23, 1996.
Horne, W. B.; Phillips,
W. P.; Sparks, H. C.; and Yager, T. J.: A Comparison
of Aircraft and Ground Vehicle Stopping Performance
on Dry, Wet, Flooded, Slush-, Snow-, and Ice-Covered
Runways. NASA TN D 6098, 1970.
Jones, Lisa E.; and Carden,
Huey D.: Overview of Structural Behavior and
Occupant Responses From a Crash Test of a Composite
Airplane. NASA TM-111954, 1995. (Also available
as SAE Paper 951168.)
Joyner, Upshur T.; Phillips, W. Pelham; and Yager,
Thomas J.: Recent Studies on Effects of Runway
Grooving on Airplane Operations. AIAA Paper 69-773,
1969.
Lewis, M. S.; Robinson,
P. A.; Hinton, D. A.; and Bowles, R. L.: The
Relationship of an Integral Wind Shear Hazard to
Aircraft Performance Limitations. NASA TM-109080,
1994.
Patterson, J. C., Jr.;
and Jordan, F. L., Jr.: A Static Air Flow Visualization
Method To Obtain a Time History of the Lift-Induced
Vortex and Circulation. NASA TM X-72769, 1975.
Pitts, Felix L.; Lee, Larry
D.; Perala, Rodney A.; and Rudolph, Terence H.:
New Methods and Results for Quantification of
Lightning-Aircraft Electrodynamics. NASA TP-2737,
1987.
Pitts, Felix L.; and Thomas,
Mitchel E.: In-Flight Direct-Strike Lightning Research.
1980 Aircraft Safety and Operating Problems.
Joseph W. Stickle, compiler, NASA CP-2170, Pt.
1, 1981, pp. 359–372.
Proctor, F. H.; Bracalente,
E. M.; Harrah, S. D.; Switzer, G. F.; and Britt,
C. L., Jr.: Simulation of the 1994 Charlotte Microburst
With Look-Ahead Windshear Radar. 27th Conference
on Radar Meteorology, American Meteorol. Soc.,
1995, pp. 530–532.
Proctor, Fred H.: The NASA-Langley Wake Vortex
Modelling Effort in Support of an Operational Aircraft
Spacing System. AIAA Paper 98-0589, 1998.
Proctor, Fred H.; Hinton,
David A.; and Bowles, Roland L.: A Windshear Hazard
Index. Ninth Conference on Aviation, Range and
Aerospace Meteorology, American Meteorol. Soc.,
2000, pp. 482–487.
Pryzby, J. E.; and Plumer,
J. A.: Lightning Protection Guidelines and Test
Data for Adhesively Bonded Aircraft Structures.
NASA CR-3762, 1984.
Stewart, Eric C.: A Piloted Simulation Study of
Wake Turbulence on Final Approach. AIAA Paper 98-4339,
1998.
Stough, H. P., III; Greene, George C.; Stewart,
Eric C.; Stuever, Robert A., Jordan, Frank L.,
Jr.; Rivers, Robert A.; and Vicroy, Dan D.: NASA
Wake Vortex Research. AIAA Paper 93-4004, 1993.
Stuever, Robert A.; and Stewart, Eric C.: The Role
of Simulation in Determining Safe Aircraft Landing
Separation Criteria. Presented at the FAA International
Wake Vortex Symposium (Washington, D.C.), Oct.
29–31, 1991.
Switzer, G. F.; Proctor,
F. H.; Hinton, D. A.; and Aanstoos, J. V.: Windshear
Database for Forward-Looking Systems Certification.
NASA TM-109012, 1993.
Tatnall, C. R.: A Proposed Methodology for Determining
Wake-Vortex Imposed Aircraft Separation Constraints.
M.S. Thesis, George Washington University, Aug.
1995.
Terry, James E.: Design and Test of an Improved
Crashworthiness Small Composite Airframe. SAE Paper
2000-01-1673, 2000.
Thompson, William C.: Model
Ditching Investigation of the Boeing 707 Jet Transport.
NACA RM SL55K08, Civil Aeronautics Administration,
1955.
Thomson, Robert G.; Carden,
Huey D.; and Hayduk, Robert J.: Survey of NASA
Research on Crash Dynamics. NASA TP-2298, 1984.
Vaughan, Victor L., Jr.;
and Alfaro-Bou, Emilio: Impact Dynamics Research
Facility for Full-Scale Aircraft Crash Testing.
NASA TN D-8179, 1976.
Wallace, Lane E.: Airborne
Trailblazer: Two Decades With NASA Langley’s
737 Flying Laboratory. NASA SP-4216, 1994.
Yager, T. J.; and White,
E. J.: Recent Progress Toward Predicting Aircraft
Ground Handling Performance. 1980 Aircraft Safety
and Operating Problems, Joseph W. Stickle,
compiler, NASA CP-2170, Pt. 2, 1981, pp. 583–611.
Yager, Thomas J.; and White,
Ellis J.: Recent Progress Towards Predicting
Aircraft Ground Handling Performance. NASA
TM-81952, 1981.
Flight Systems
Abbott, Terence S.: A
Simulation Evaluation of the Engine Monitoring
and Control System Display. NASA TP-2960, 1990.
Bortolussi, Michael R.:
An Investigation of General Aviation Problems
and Issues: An Integration of Pilot-Cockpit Interface
Research. NASA/CR-97-113005, 1997.
Knox, Charles E.; and Scanlon,
Charles H.: Flight Tests With a Data Link Used
for Air Traffic Control Information Exchange.
NASA TP-3135, 1991.
Lambregts, Anthony A.; and Creedon, Jeremiah F.:
Development and Flight Evaluation of Automatic
Flare Laws With Improved Touchdown Dispersion.
AIAA Paper 80-1757, 1980.
Morello, Samuel A.: Recent
Flight Test Results Using an Electronic Display
Format on the NASA B-737. Guidance and Control
Design Considerations for Low-Altitude and Terminal-Area
Flight, AGARD-CP-240, Apr. 1978, pp. 16-1–16-10.
(Available from DTIC as AD-A057177.)
Morello, Samuel A.; Knox,
Charles E.; and Steinmetz, George G.: Flight-Test
Evaluation of Two Electronic Display Formats for
Approach to Landing Under Instrument Conditions.
NASA TP-1085, 1977.
Person, Lee H., Jr.; and Steinmetz, George G.:
The Integration of Control and Display Concepts
for Improved Pilot Situational Awareness. Presented
at the Flight Safety Foundation 34th International
Air Safety Seminar, Nov. 9–12, 1981.
Person, Lee H., Jr.; and Yenni, Kenneth R.: Flying
NASA’s Terminal Configured Vehicle Against
the Microwave Landing System. Paper presented to
the Society of Experimental Test Pilots, 1978.
(Unpublished)
Reeder, John P.; Schmitz,
Robert A.; and Clark, Leonard V.: Operational
Benefits From the Terminal Configured Vehicle.
NASA TM-80046, 1979.
Reeder, John P.; Taylor,
Robert T.; and Walsh, Thomas M.: New Design
and Operating Techniques and Requirements for Improved
Aircraft Terminal Area Operations. NASA TM
X-72006, 1974. (Also available as SAE Paper 740454.)
Stough, H. Paul, III; Shafer, Daniel B.; Schaffner,
Philip R.; and Martzaklis, Konstantinos S.: Reducing
Aviation Weather-Related Accidents Through High-Fidelity
Weather Information Distribution and Presentation.
ICAS Paper 2000-6.5.1, 2000.
Wallace, Lane E.: Airborne
Trailblazer: Two Decades With NASA Langley’s
737 Flying Laboratory. NASA SP-4216, 1994.
Walsh, Thomas M.; Morello,
Samuel A.; and Reeder, John P.: Review of Operational
Aspects of Initial Experiments Utilizing the U.S.
MLS. Aircraft Safety and Operating Problems,
NASA SP-416, 1976, pp. 3–19.
Structures and Materials
Anon.: Risk to the Public
From Carbon Fibers Released in Civil Aircraft Accidents.
NASA SP-448, 1980.
Bell, Vernon L.: The
Potential for Damage From the Accidental Release
of Conductive Carbon Fibers From Burning Composites.
NASA TM-80213, 1980.
Buffum, Harvey E.; and
Thompson, Vere S.: Transition From Glass to Graphite
in Manufacture of Composite Aircraft Structure.
CTOL Transport Technology—1978, NASA
CP-2036, Pt. 1, 1978, pp. 331–347.
Davis, John G., Jr.: Overview
of the ACT Program. Ninth DOD/NASA/FAA Conference
on Fibrous Composites in Structural Design,
Vol. 2, Joseph R. Soderquist, Lawrence M. Neri,
and Herman L. Bohon, compilers, NASA CR-198722,
1992, pp. 577–599.
Davis, John G., Jr.; Starnes,
James H., Jr.; and Johnston, Norman J.: Advanced
Composites Research and Development for Transport
Aircraft. 17th ICAS Congress, Vol. 1, 1990,
pp. XLV–LIV.
Dexter, H. Benson: Long-Term
Environmental Effects and Flight Service Evaluation
of Composite Materials. NASA TM-89067, 1987.
Dexter, H. Benson; Harris,
Charles E.; and Johnston, Norman J.: Recent Progress
in NASA Langley Research Center Textile Reinforced
Composites Program. Second NASA Advanced Composites
Technology Conference, John G. Davis, Jr.,
and Herman L. Bohon, compilers, NASA CP-3154, 1992,
pp. 295–323.
Dow, Marvin B.: The
ACEE Program and Basic Composites Research at Langley
Research Center (1975–1986)—Summary
and Bibliography. NASA RP-1177, 1987.
Dow, Marvin B.; and Dexter,
H. Benson: Development of Stitched, Braided
and Woven Composite Structures in the ACT Program
and at Langley Research Center. NASA TP-97-206234,
1997.
Ethell, Jeffrey L.: Fuel
Economy in Aviation. NASA SP-462, 1983.
Harris, Charles E.; and Heyman, Joseph S.: An Overview
of NASA Research Related to the Aging Commercial
Transport Fleet. AIAA Paper 91-0952, 1991.
Harris, Charles E.; and
Poe, Clarence C., Jr.: Role of Mechanics of Textile
Preform Composites in the NASA Advanced Composites
Technology Program. Mechanics of Textile Composites
Conference, Clarence C. Poe, Jr., and Charles
E. Harris, eds., NASA CP-3311, Pt. 1, 1995, pp.
1–4.
Harris, Charles E.; Starnes,
James H., Jr.; and Shuart, Mark J.: An Assessment
of the State-of-the-Art in the Design and Manufacturing
of Large Composite Structures for Aerospace Vehicles.
NASA TM-2001-210844, 2001.
Pride, Richard A.: Large-Scale
Carbon Fiber Tests. NASA TM-80218, 1980.
Pride, Richard A.: Environmental
Effects on Composites for Aircraft. CTOL Transport
Technology—1978, NASA CP-2036, Pt. 1,
1978, pp. 239–258.
Stauffer, Warren A.; and
James, Arthur M.: Development of Advanced Composite
Structures. CTOL Transport Technology—1978,
NASA CP-2036, Pt. 1, 1978, pp. 259–279.
Stone, M.: Key Issues in
Application of Composites to Transport Aircraft.
CTOL Transport Technology—1978, NASA
CP-2036, Pt. 1, 1978, pp. 281–310.
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