EBookClubs

Read Books & Download eBooks Full Online

EBookClubs

Read Books & Download eBooks Full Online

Book Wind tunnel Investigation at High Subsonic Speeds of the Static Longitudinal Stability Characteristics of a Complete Model Having Cropped delta  Swept  and Unswept Wings and Several Horizontal tail Heights

Download or read book Wind tunnel Investigation at High Subsonic Speeds of the Static Longitudinal Stability Characteristics of a Complete Model Having Cropped delta Swept and Unswept Wings and Several Horizontal tail Heights written by Kenneth W. Goodson and published by . This book was released on 1954 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Static Longitudinal Characteristics at High Subsonic Speeds of a Complete Airplane Model with a Highly Tapered Wing Having the 0 80 Chord Line Unswept and with Several Tail Configurations

Download or read book Static Longitudinal Characteristics at High Subsonic Speeds of a Complete Airplane Model with a Highly Tapered Wing Having the 0 80 Chord Line Unswept and with Several Tail Configurations written by Kenneth W. Goodson and published by . This book was released on 1961 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made at high subsonic speeds of a complete model having a highly tapered wing and several tail configurations. The basic aspect-ratio-4.00 wing had a zero taper and an unswept 0.80 chord line. Several aspect-ratio modifications to the basic wing were made by clipping off portions of the wing tips. The complete model was tested with a chord-plane tail, a T-tail, and a biplane tail (combined T-tail and chord-plane tail). The model was tested in the Langley high-speed 7- by 10-foot tunnel at Mach numbers from 0.60 to 0.92. The data show that, when reduced to the same static margin, all the tail configurations tested on the model provided fairly good stability characteristics, the biplane tail giving the best overall characteristics as regards pitching-moment linearity. Changes in static margin at zero lift coefficient with Mach number were small for the model with these tails over the Mach number range investigated.

Book Index of NACA Technical Publications

Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1959 with total page 388 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Selected Listing of NASA Scientific and Technical Reports for

Download or read book A Selected Listing of NASA Scientific and Technical Reports for written by and published by . This book was released on 1954 with total page 818 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Design Guide for Pitch up Evaluation and Investigation at High Subsonic Speeds of Possible Limitations Due to Wing aspect ratio Variations

Download or read book Design Guide for Pitch up Evaluation and Investigation at High Subsonic Speeds of Possible Limitations Due to Wing aspect ratio Variations written by Kenneth P. Spreemann and published by . This book was released on 1959 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Technical Note

    Book Details:
  • Author :
  • Publisher :
  • Release : 1961
  • ISBN :
  • Pages : 498 pages

Download or read book NASA Technical Note written by and published by . This book was released on 1961 with total page 498 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book WADC Technical Report

Download or read book WADC Technical Report written by United States. Wright Air Development Division and published by . This book was released on 1957 with total page 1268 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Index of N A S A Technical Publications

Download or read book Index of N A S A Technical Publications written by United States. National Aeronautics and Space Administration and published by . This book was released on 1960 with total page 448 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Research Abstracts and Reclassification Notice

Download or read book Research Abstracts and Reclassification Notice written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1954 with total page 508 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Low speed Investigation of Static Longitudinal and Lateral Stability Characteristics of an Airplane Configuration with a Highly Tapered Wing and with Several Body and Tail Arrangements

Download or read book Low speed Investigation of Static Longitudinal and Lateral Stability Characteristics of an Airplane Configuration with a Highly Tapered Wing and with Several Body and Tail Arrangements written by Paul G. Fournier and published by . This book was released on 1960 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Index to NASA Technical Publications

Download or read book Index to NASA Technical Publications written by United States. National Aeronautics and Space Administration and published by . This book was released on 1960-07 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Monthly Catalog of United States Government Publications

Download or read book Monthly Catalog of United States Government Publications written by United States. Superintendent of Documents and published by . This book was released on 1956 with total page 1640 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerodynamic Studies

Download or read book Aerodynamic Studies written by Zbigniew Krzywoblocki (|d) and published by . This book was released on 1957 with total page 170 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Subject Index to Unclassified ASTIA Documents

Download or read book Subject Index to Unclassified ASTIA Documents written by Defense Documentation Center (U.S.) and published by . This book was released on 1960 with total page 296 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Wind tunnel Investigation at High Subsonic Speeds of Some Effects of Fuselage Cross section Shape and Wing Height on the Static Longitudinal and Lateral Stability Characterisitcs of a Model Having a 45 Degree Swept Wing

Download or read book Wind tunnel Investigation at High Subsonic Speeds of Some Effects of Fuselage Cross section Shape and Wing Height on the Static Longitudinal and Lateral Stability Characterisitcs of a Model Having a 45 Degree Swept Wing written by Thomas J. Jr King and published by . This book was released on 1956 with total page 61 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Wind tunnel Investigation at Subsonic and Supersonic Speeds of Static and Dynamic Stability Derivatives of Airplane Model with Unswept Wing and High Horizontal Tail  with List of References

Download or read book Wind tunnel Investigation at Subsonic and Supersonic Speeds of Static and Dynamic Stability Derivatives of Airplane Model with Unswept Wing and High Horizontal Tail with List of References written by and published by . This book was released on 1959 with total page 77 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Some Lessons Learned with Wind Tunnels

Download or read book Some Lessons Learned with Wind Tunnels written by and published by . This book was released on 1986 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: