1) STEP and STEPSPL--computer programs for aerodynamic model structure determination and parameter estimation

Author
Batterson, James G
Publisher
National Aeronautics and Space Administration, Langley Research Center
Pub. Date
[1986]
Language
English

2) Flow-visualization techniques used at high speed by configuration aerodynamics wind-tunnel-test team

Series
NASA technical memorandum volume 210848
Publisher
Available from NASA Center for AeroSpace Information (CASI)
Pub. Date
[2001]
Language
English

3) High Reynolds number investigation of a flush-mounted, S-duct inlet with large amounts of boundary layer ingestion

Author
Berrier, Bobby L
Series
NASA technical paper volume 2005-213766
Publisher
National Aeronautics and Space Administration, Langley Research Center
Pub. Date
[2005]
Language
English

4) Nonlinear aerodynamic wing design

Author
Bonner, Ellwood
Series
NASA contractor report volume NASA CR-3950
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Branch
Pub. Date
December 1985.
Language
English

5) Super cooled large droplet analysis of several geometries using LEWICE3D version 3

Author
Bidwell, Colin S
Series
NASA technical memorandum volume 2011-216945
Publisher
National Aeronautics and Space Administration, Glenn Research Center
Pub. Date
[2011]
Language
English

6) Use of constrained optimization in the conceptual design of a medium-range subsonic transport

Author
Sliwa, Steven M
Series
NASA technical paper volume 1762
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Branch
Pub. Date
December 1980.
Language
English

7) Design of fuselage shapes for natural laminar flow

Author
Dodbele, S. S
Series
NASA contractor report volume NASA CR-3970
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Branch
Pub. Date
March 1986.
Language
English

8) Damage arresting composites for shaped vehicles: phase II final report

Series
NASA contractor report volume NASA CR-216880
Publisher
National Aeronautics and Space Administration, Langley Research Center
Pub. Date
[2011]
Language
English

9) Flutter analysis of a transonic fan

Author
Srivastava, R
Series
NASA technical memorandum volume 2002-211818
Publisher
National Aeronautics and Space Administration, Glenn Research Center
Pub. Date
September 2002.
Language
English

10) Flow prediction for propfan engine installation effects on transport aircraft at transonic speeds

Author
Samant, S. S
Series
NASA contractor report volume NASA CR-3954
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Branch
Pub. Date
January 1986.
Language
English

11) Recent improvements to the Acoustical Testing Laboratory at the NASA Glenn Research Center

Author
Podboy, Devin M
Series
NASA technical memorandum volume 2014-218110
Publisher
National Aeronautics and Space Administration, Langley Research Center
Pub. Date
March 2014.
Language
English

12) Full potential methods for analysis/design of complex aerospace configurations

Author
Shankar, Vijaya
Series
NASA contractor report volume NASA CR-3982
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Branch
Pub. Date
May 1986.
Language
English

13) Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63

Author
Pittman, Jimmy L
Series
NASA technical paper volume 1767
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Branch
Pub. Date
December 1980.
Language
English

14) Flutter analysis of a transonic fan

Series
NASA technical memorandum volume 211818
Publisher
National Aeronautics and Space Administration, Glenn Research Center
Pub. Date
2002]
Language
English

15) Method for the prediction of the installation aerodynamics of a propfan at subsonic speeds: user manual

Author
Chandrasekaran, B
Series
NASA contractor report volume NASA CR-178057
Publisher
National Aeronautics and Space Administration, Langley Research Center
Pub. Date
[1986]
Language
English

16) Use of hyperbolic grid generation scheme in simulating supersonic viscous flow about three-dimensional winged configurations

Author
Rizk, Yehia M
Series
NASA technical memorandum volume 86776
Publisher
National Aeronautics and Space Administration, Ames Research Center
Pub. Date
July 1985.
Language
English

17) Hybrid wing body shielding studies using an ultrasonic configurable fan artificial noise source generating typical turbofan modes

Author
Sutliff, Daniel L
Series
NASA technical memorandum volume 218119
Publisher
National Aeronautics and Space Administration, Glenn Research Center
Pub. Date
April 2014.
Language
English

18) Dynamic assessment of B-52B-008 carrier aircraft for the revised space shuttle solid rocket booster decelerator subsystem drop test vehicle

Author
Doty, Leslie J
Series
NASA contractor report volume NASA CR-170989
Publisher
National Aeronautics and Space Administration
Pub. Date
[December 16, 1983]
Language
English

19) NASA N+3 subsonic fixed wing silent efficient low-emissions commercial transport (SELECT) vehicle study, revision a

Series
NASA contractor report volume NASA CR-216798
Publisher
National Aeronautics and Space Administration, Glenn Research Center
Pub. Date
[2010]
Language
English

20) Large-scale advanced prop-fan (LAP) blade design

Author
Sullivan, William E
Publisher
Hamilton Standard Division, United Technologies
Pub. Date
[1984?]
Language
English