Technical Publications Home
Technical Publications Manual
Dryden Technical Report Server
1946-2006 Dryden Bibliography
Report Server FAQ
Dryden Research Library
NASA Scientific and Technical Information
NASA Research Resources
Additional Resources
Number of records: 17.
Roman, James and Sato, Robert N. (1967) A Useful Modification of the Wright Spirometer. Technical Report NASA Technical Note TN D-4234, Research Engineering, NASA Dryden Flight Research Center.
Taylor Jr., Lawrence W. and Smith, John W. (1967) An Analysis of the Limit-Cycle and Structural-Resonance Characteristics of the X-15 Stability Augmentation System. Technical Report NASA Technical Note TN D-4287, Research Engineering, NASA Dryden Flight Research Center.
Matranga, Gene J. and Mallick, Donald L. and Kluever, Emil E. (1967) An Assessment of Ground and Flight Simulators for the Examination of Manned Lunar Landing. Conference Paper AIAA-1967-238, Research Engineering, NASA Flight Research Center.
Thompson, Milton O. and Weil, Joseph and Holleman, Euclid C. (1967) An Assessment of Lifting Reentry Flight Control Requirements During Abort, Terminal Glide, and Approach and Landing Situations. Technical Report NASA TM X-59119, Research Engineering, NASA Dryden Flight Research Center.
McDonald, Robert T. and Roman, James (1967) Development of Respiration-Rate Transducers for Aircraft Environments. Technical Report NASA Technical Note TN D-4217, Research Engineering, NASA Dryden Flight Research Center.
Lytton, Lee E. (1967) Evaluation of a Vertical-Scale, Fixed-Index Instrument Display Panel for the X-15 Airplane. Technical Report NASA Technical Note TN D-3967, Research Engineering, NASA Dryden Flight Research Center.
Garringer, Darwin J. and Saltzman, Edwin J. (1967) Flight Demonstration of a Skin-Friction Gage to a Local Mach Number of 4.9. Technical Report NASA Technical Note TN D-3830, Research Engineering, NASA Dryden Flight Research Center.
Saltzman, Edwin J. and Hintz, John (1967) Flight Evaluation of Splitter-Plate Effectiveness in Reducing Base Drag at Mach Numbers from 0.65 to 0.90. Technical Report NASA TM X-1376, Research Engineering, NASA Dryden Flight Research Center.
Perry, John J. and Dana, William H. and Bacon Jr., Donald C. (1967) Flight Investigation of the Landing Task in a Jet Trainer with Restricted Fields of View. Technical Report NASA Technical Note TN D-4018, Research Engineering, NASA Dryden Flight Research Center.
Jarvis, Calvin R. (1967) Flight-Test Evaluation of an On-Off Rate Command Attitude Control System of a Manned Lunar-Landing Research Vehicle. Technical Report NASA Technical Note TN D-3903, Research Engineering, NASA Dryden Flight Research Center.
Jarvis, Calvin R. (1967) Fly-By-Wire Flight Control System Experience with a Free-Flight Lunar-Landing Research Vehicle. Conference Paper AIAA-1967-273, Research Engineering, NASA Flight Research Center.
Pyle, Jon S. and Swanson, Robert H. (1967) Lift and Drag Characteristics of the M2-F2 Lifting Body During Subsonic Gliding Flight. Technical Report NASA TM X-1431, Research Engineering, NASA Dryden Flight Research Center.
Kordes, Eldon E. and Love, Betty J. (1967) Preliminary Evaluation of XB-70 Airplane Encounters with High-Altitude Turbulence. Technical Report NASA Technical Note TN D-4209, Research Engineering, NASA Dryden Flight Research Center.
Wilson, Ronald J. (1967) Statistical Analysis of Landing Contact Conditions of the X-15 Airplane. Technical Report NASA Technical Note TN D-3801, Research Engineering, NASA Dryden Flight Research Center.
Wilson, Ronald J. and Larson, Richard R. (1967) Statistical Analysis of Landing-Contact Conditions for the XB-70 Airplane. Technical Report NASA Technical Note TN D-4007, Research Engineering, NASA Dryden Flight Research Center.
Szalai, Kenneth J. (1967) The Influence of Response Feedback Loops on the Lateral-Directional Dynamics of a Variable-Stability Transport Aircraft. Technical Report NASA Technical Note TN D-3966, Research Engineering, NASA Dryden Flight Research Center.
Montoya, Earl J. and Palitz, Murray (1967) Wind-Tunnel Investigation of the Flow Field Beneath the Fuselage of the X-15 Airplane at Mach Numbers from 4 to 8. Technical Report NASA TM X-1469, Research Engineering, NASA Dryden Flight Research Center.
This list was generated on Wed Aug 27 18:17:51 PDT 2008.
Last Modified: September 14, 2004 Responsible NASA Official: Jenny Baer-Riedhart Webmasters
NASA Web Privacy Statement