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Online Books by

Hugh L. Dryden Flight Research Center

Books from the extended shelves:

• Hugh L. Dryden Flight Research Center: Advanced control technology and its potential for future transport aircraft (U.S. National Aeronautics and Space Administration ;, 1976), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Aerodynamic derivatives for an oblique wing aircraft estimated from flight data by using a maximum likelihood technique (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Richard E. Maine and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Analytical study of a free-wing/free-trimmer concept (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Richard F. Porter, Battelle Memorial Institute. Columbus Laboratories, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Application of a performance modeling technique to an airplane with variable sweep wings (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Paul C. Redin and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Boundary-layer transition correlation on a slender cone in wind tunnels and flight for indications of flow quality (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1982., 1982), also by N. Sam Dougherty, David F. Fisher, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: A characterization of the real zeros of a particular transcendental function (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by David R. Hedgley and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Comparison of calculated and altitude-facility-measured thrust and airflow of two prototype F100 turbofan engines (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Frank J. Kurtenbach and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Comparison of concurrent strain gage- and presure transducer-measured flight loads on a lifting reentry vehicle and correlation with wind tunnel predictions (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Ming Han Tang, Robert G. Sheldon, Walter J. Sefic, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Comparison of three thrust calculation methods using in-flight thrust data (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Donald L. Hughes and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Determination of subcritical frequency and damping from B-1 flight flutter test data (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Steven Kent Dobbs, C. H. Hodson, and Rockwell International. Los Angeles Aircraft Division (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Development and flight test results of an autothrottle control system at Mach 3 cruise (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Glenn B. Gilyard, John J. Burken, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Diversity techniques for omnidirectional telemetry coverage of the HiMAT research vehicle (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Paul F. Harney and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Effect of an alternate winglet on the pressure and spanwise load distributions of a first-generation jet transport wing (National Aeronautics and Space Administration, Scientific and Technical Information Association ;, 1978), also by Lawrence C. Montoya, Peter F. Jacobs, Stuart G. Flechner, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Effect of number of probes and their orientation on the calculation of several compressor face distortion descriptors (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Frederick Stoll, Henry H. Arnaiz, Jeffrey W. Tremback, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Effects of fuselage forebody geometry on low-speed lateral-directional characteristics of twin-tail fighter model at high angles of attack (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Peter C. Carr, William P. Gilbert, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: An efficient code for the simulation of nonhydrostatic stratified flow over obstacles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Gregory G. Pihos, Morton G. Wurtele, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Elastic constants for superplastically formed/diffusion bonded corrugated sandwich core (National Aeronautics and Space Administration, 1980), also by William L. Ko, E. S. Harrison, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Evaluation of a simplified gross thrust calculation technique using two prototype F100 turbofan engines in an altitude facility (National Aeronautics and Space Administration, Scientific and Technical Information Branch :, 1979), also by Frank J. Kurtenbach and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Experimental and numerical characterization of a steady-state cylindrical blackbody cavity at 1100 degrees celsius (NASA, Dryden Flight Research Center, 2000), also by Thomas J. Horn, Amanie N. Abdelmessih, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Extended analytical study of the free-wing/free-trimmer concept (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Richard F. Porter, Rodolfo D. Vergara, David W. Hall, Battelle Memorial Institute. Columbus Laboratories, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Flight comparison of the transonic agility of the F-111A airplane and the F-111 supercritical wing airplane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Edward L. Friend, Glenn M. Sakamoto, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Flight-determined stability and control derivatives for the F-111 TACT research aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Service ;, 1978), also by Alex G. Sim, Robert E. Curry, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Frank J. Kurtenbach, Frank W. Burcham, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Louis L. Steers and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Historical background and design evolution of the transonic aircraft technology supercritical wing (National Aeronautical and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Theodore G. Ayers, James B. Hallissy, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Important factors in the maximum likelihood analysis of flight test maneuvers (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Kenneth W. Iliff, T. D. Montgomery, Richard E. Maine, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Improved test methods for determining lightning-induced voltages in aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by K. E. Crouch, J. A. Plumer, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Robert D. Quinn, Leslie Gong, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Landing approach airframe noise measurement and analysis (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Paul L. Lasagna and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Limited evaluation of an F-14A airplane utilizing an aileron-rudder inter-connect control system in the landing configuration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Wendell W. Kelley, Einar K. Enevoldson, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: A modified T-value method for selection of strain gages for measuring loads on a low aspect ratio wing (National Aeronautics and Space Administration, Scientific and Technical Informaion Branch;, 1980), also by Ming Han Tang, Robert G. Sheldon, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Practical aspects of using a maximum likelihood estimation method to extract stability and control derivitives from flight data (National Aeronautics and Space Administration ;, 1976), also by Kenneth W. Iliff, Richard E. Maine, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Precision controllability of the F-15 airplane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Thomas R. Sisk, Neil W. Matheny, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Precision controllability of the YF-17 airplane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Thomas R. Sisk, Neil W. Matheny, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Programmer's manual for MMLE3, a general FORTRAN program for maximum likelihood parameter estimation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Richard E. Maine and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Similitude requirements and scaling relationships as applied to model testing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Chester H. Wolowicz, William P. Gilbert, James S. Bowman, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Stability and control of the Gossamer human-powered aircraft by analysis and flight test (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Henry R. Jex, David G. Mitchell, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and inc Systems Technology (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Subsonic tests of an all-flush-pressure-orifice air data system (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Terry J. Larson, Paul M. Siemers, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: User's manual for MMLE3, a general FORTRAN program for maximum likelihood parameter estimation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Richard E. Maine, Kenneth W. Iliff, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Hugh L. Dryden Flight Research Center: Wind tunnel investigation of an all flush orifice air data system for a large subsonic aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Terry J. Larson, Paul M. Siemers, Stuart G. Flechner, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)

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