WorldCat Identities

United States National Aeronautics and Space Administration Scientific and Technical Information Program

Overview
Works: 1,236 works in 1,961 publications in 1 language and 103,063 library holdings
Genres: Periodicals  Conference papers and proceedings  Biography  Abstracts  Bibliography 
Roles: isb
Classifications: Z6664.3, 629.1092273
Publication Timeline
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Most widely held works about United States
 
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Most widely held works by United States
NASA engineers and the age of Apollo by Sylvia Doughty Fries( Book )

4 editions published in 1992 in English and held by 587 WorldCat member libraries worldwide

Scientific and technical aerospace reports( )

in English and held by 458 WorldCat member libraries worldwide

Aerospace medicine and biology( )

in English and held by 448 WorldCat member libraries worldwide

A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
Proceedings of the ... Space Photovoltaic Research and Technology Conference by Space Photovoltaic Research and Technology Conference( )

in English and held by 430 WorldCat member libraries worldwide

Space resources by United States( Book )

3 editions published in 1992 in English and held by 386 WorldCat member libraries worldwide

STI bulletin( )

in English and held by 345 WorldCat member libraries worldwide

This publication provides feature stories about the activities of the NASA Scientific and Technical Information (STI) Program
Aeronautical engineering( )

in English and held by 334 WorldCat member libraries worldwide

A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Sscientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
Proceedings of a symposium by Aerospace Mechanisms Symposium( )

in English and held by 318 WorldCat member libraries worldwide

Issues in NASA program and project management by Francis T Hoban( Book )

4 editions published between 1991 and 1993 in English and held by 308 WorldCat member libraries worldwide

NASA thesaurus by United States( )

in English and held by 288 WorldCat member libraries worldwide

Workshop on Squeezed States and Uncertainty Relations : proceedings of a workshop held at the University of Maryland, College Park, Maryland, March 28-30, 1991 by D Han( Book )

3 editions published in 1992 in English and held by 156 WorldCat member libraries worldwide

Probabilistic micromechanics and macromechanics for ceramic matrix composites by P. L. N Murthy( Book )

2 editions published in 1997 in English and held by 107 WorldCat member libraries worldwide

A gas chromatograph/mass spectrometer system for ultralow-emission combustor exhaust studies by Chowen Chou Wey( Book )

2 editions published in 1996 in English and held by 103 WorldCat member libraries worldwide

Supersonic flying qualities experience using the SR-71 by Timothy H Cox( Book )

5 editions published in 1997 in English and held by 97 WorldCat member libraries worldwide

Approximately 25 years ago NASA Dryden Flight Research Center, Edwards, California, initiated the evaluation of supersonic handling qualities issues using the XB-70 and the YF-12. Comparison of pilot comments and ratings with some of the classical handling qualities criteria for transport aircraft provided information on the usefulness of these criteria and insight into supersonic flying qualities issues. A second research study has recently been completed which again addressed supersonic flying qualities issues through evaluations of the SR-71 in flight at Mach 3. Additional insight into supersonic flying qualities issues was obtained through pilot ratings and comments. These ratings were compared with existing military specifications and proposed criteria for the High Speed Civil Transport. This paper investigates the disparity between pilot comments and the Neal/Smith criteria through a modification of the technique using vertical speed at the pilot station. The paper specifically addresses the pilot ability to control flightpath and pitch attitude in supersonic flight and pilot displays typical of supersonic maneuvering
A model for Space Shuttle orbiter tire side forces based on NASA Landing Systems Research Aircraft test results by John F Carter( Book )

2 editions published in 1997 in English and held by 95 WorldCat member libraries worldwide

High-alpha handling qualities flight research on the NASA F/A-18 High Alpha Research Vehicle by Keith D Wichman( Book )

2 editions published in 1996 in English and held by 94 WorldCat member libraries worldwide

A flight research study of high-angle-of-attack handling qualities has been conducted at the NASA Dryden Flight Research Center using the F/A-18 High Alpha Research Vehicle (HARV). The objectives were to create a high-angle-of-attack handling qualities flight database, develop appropriate research evaluation maneuvers, and evaluate high-angle-of-attack handling qualities guidelines and criteria. Using linear and nonlinear simulations and flight research data, the predictions from each criterion were compared with the pilot ratings and comments. Proposed high-angle-of-attack nonlinear design guidelines and proposed handling qualities criteria and guidelines developed using piloted simulation were considered. Recently formulated time-domain Neal-Smith guidelines were also considered for application to high-angle-of-attack maneuvering. Conventional envelope criteria were evaluated for possible extension to the high-angle-of-attack regime. Additionally, the maneuvers were studied as potential evaluation techniques, including a limited validation of the proposed standard evaluation maneuver set. This paper gives an overview of these research objectives through examples and summarizes result highlights. The maneuver development is described briefly, the criteria evaluation is emphasized with example results given, and a brief discussion of the database form and content is presented
Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV by David F Fisher( Book )

2 editions published in 1996 in English and held by 94 WorldCat member libraries worldwide

Least squares best fit method for the three parameter Weibull distribution : analysis of tensile and bend specimens with volume or surface flaw failure by Bernard Gross( Book )

2 editions published in 1996 in English and held by 92 WorldCat member libraries worldwide

Structural dynamic model obtained from flight use with piloted simulation and handling qualities analysis by Bruce G Powers( Book )

2 editions published in 1996 in English and held by 92 WorldCat member libraries worldwide

Flight test of a propulsion-based emergency control system on the MD-11 airplane with emphasis on the lateral axis by John J Burken( Book )

2 editions published in 1996 in English and held by 92 WorldCat member libraries worldwide

A large, civilian, multiengine transport MD-11 airplane control system was recently modified to perform as an emergency backup controller using engine thrust only. The emergency backup system, referred to as the propulsion-controlled aircraft (PCA) system, would be used if a major primary flight control system fails. To allow for longitudinal and lateral-directional control, the PCA system requires at least two engines and is implemented through software modifications. A flight-test program was conducted to evaluate the PCA system high-altitude flying characteristics and to demonstrate its capacity to perform safe landings. The cruise flight conditions, several low approaches and one landing without any aerodynamic flight control surface movement, were demonstrated. This paper presents results that show satisfactory performance of the PCA system in the longitudinal axis. Test results indicate that the lateral-directional axis of the system performed well at high altitude but was sluggish and prone to thermal upsets during landing approaches. Flight-test experiences and test techniques are also discussed with emphasis on the lateral-directional axis because of the difficulties encountered in flight test
 
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Audience Level
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Audience level: 0.50 (from 0.42 for NASA engin ... to 0.89 for STI bullet ...)

Alternative Names

controlled identityUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division (1987-1990)

controlled identityUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Office (1992- )

N.A.S.A. S.T.I. Program

NASA STI Program

United States. National Aeronautics and Space Administration. Division of Information Resources Management. Scientific and Technical Information Program

United States. National Aeronautics and Space Administration. Office of Management. Scientific and Technical Information Program

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program Office

Languages
English (75)