Results 1 - 20 of 143 for All Library Resources
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| Result Number | Material Type | Add to My Shelf Action | Record Details and Options |
|---|---|---|---|
| 1 |
Material Type: Reports
|
|
DEVELOPMENT OF A NUMERICAL PROCEDURE FOR THE DETERMINATION OF FLUTTER CHARACTERISTICS OF LOW-ASPECT-RATIO WINGSAPPROVED FOR PUBLIC RELEASEDigital Resources/Online E-Resources |
| 2 |
Material Type: Reports
|
|
THEORETICAL STUDIES OF THE EFFECTS OF ASPECT RATIO ON FLUTTERApproved for public release; distribution is unlimited. Document partially illegible.Digital Resources/Online E-Resources |
| 3 |
Material Type: Reports
|
|
(UNCLASSIFIED TITLE) TESTS OF 5'' CHORD, ASPECT RATIO 6 HYDROFOIL USED AS A STRUT AND TESTS OF 2 1/2'' CHORD HYDROFOIL FOR VARIOUS ASPECT RATIOS IN SINGLE AND TANDEM CONFIGURATIONSAPPROVED FOR PUBLIC RELEASEDigital Resources/Online E-Resources |
| 4 |
Material Type: Reports
|
|
EXTENSION OF SINGLE AND TANDEM FOIL TESTS OF 2 1/2'' CHORD ASPECT RATIO 20 HYDROFOIL AND 5'' CHORD ASPECT RATIO 6 HYDROFOILAPPROVED FOR PUBLIC RELEASEDigital Resources/Online E-Resources |
| 5 |
Material Type: Reports
|
|
TEST OF 5'' CHORD, ASPECT RATIO 6 HYDROFOIL MODELAPPROVED FOR PUBLIC RELEASEDigital Resources/Online E-Resources |
| 6 |
Material Type: Reports
|
|
Lift, Drag, and Pitching Moment of Low-Aspect-Ratio Wings at Subsonic and Supersonic Speeds : Plane Tapered Wing of Aspect Ratio 3.1 with 3-Percent-Thick, Biconvex SectionPublic Public Domain No Copyright, Unclassified, Unlimited, Publicly availableDigital Resources/Online E-Resources |
| 7 |
Material Type: Reports
|
|
Characteristics of Low-Aspect-Ratio Wings at Supercritical Mach NumbersPublic Public Domain No Copyright, Unclassified, Unlimited, Publicly availableDigital Resources/Online E-Resources |
| 8 |
Material Type: Reports
|
|
FLUTTER ANALYSIS OF LOW ASPECT RATIO STRAIGHT WINGS IN THE TRANSONIC REGIONAPPROVED FOR PUBLIC RELEASEDigital Resources/Online E-Resources |
| 9 |
Material Type: Reports
|
|
THE TRANSONIC CHARACTERISTICS OF UNSWEPT WINGS HAVING ASPECT RATIOS OF 4, SPANWISE VARIATIONS IN THICKNESS RATIO, AND VARIATIONS IN PLAN-FORM TAPER-TRANSONIC-BUMP TECHNIQUEApproved for public release; distribution is unlimited.Digital Resources/Online E-Resources |
| 10 |
Material Type: Reports
|
|
EXPERIMENTAL INVESTIGATION OF THE EFFECTS OF PLAN-FORM TAPER ON THE AERODYNAMIC CHARACTERISTICS OF SYMMETRICAL UNSWEPT WINGS OF VARYING ASPECT RATIOApproved for public release; distribution is unlimited.Digital Resources/Online E-Resources |
| 11 |
Material Type: Reports
|
|
Stability and control characteristics of a free-flying model with an unswept wing of aspect ratio 3 (XS-3)Public Public Domain No Copyright, Unclassified, Unlimited, Publicly availableDigital Resources/Online E-Resources |
| 12 |
Material Type: Reports
|
|
Wind-Tunnel Investigation at Low Speeds of the Pitching Derivatives of Untapered Swept WingsPublic Public Domain No Copyright, Unclassified, Unlimited, Publicly availableDigital Resources/Online E-Resources |
| 13 |
Material Type: Reports
|
|
Characteristics of Low-Aspect Ratio Wings at Supercritical Mach NumbersPublic Public Domain No Copyright, Unclassified, Unlimited, Publicly availableDigital Resources/Online E-Resources |
| 14 |
Material Type: Reports
|
|
Calculations of the Supersonic Wave Drag of Nonlifting Wings with Arbitrary Sweepback and Aspect RatioApproved for public release; distribution is unlimited.Digital Resources/Online E-Resources |
| 15 |
Material Type: Reports
|
|
Drag Characteristics of Rectangular and Swept-Back NACA 65-009 Airfoils Having Various Aspect Ratios as Determined by Flight Tests at Supersonic SpeedsApproved for public release; distribution is unlimited.Digital Resources/Online E-Resources |
| 16 |
Material Type: Article
|
|
Film: The Spectator and the SpectacleAudio visual communication review, 1955-10, Vol.3 (4), p.294-300ISSN: 0885-727X ;EISSN: 2331-4052Full text available |
| 17 |
Material Type: Reports
|
|
AERODYNAMIC CHARACTERISTICS OF LOW-ASPECT-RATIO WINGS IN CLOSE PROXIMITY TO THE GROUNDAPPROVED FOR PUBLIC RELEASEDigital Resources/Online E-Resources |
| 18 |
Material Type: Reports
|
|
INVESTIGATION AT HIGH SUBSONIC SPEEDS OF THE USE OF LOW AUXILIARY TAIL SURFACES HAVING DIHEDRAL TO IMPROVE THE LONGITUDINAL AND DIRECTIONAL STABILITY OF A T-TAIL MODEL AT HIGH LIFTAPPROVED FOR PUBLIC RELEASEDigital Resources/Online E-Resources |
| 19 |
Material Type: Reports
|
|
AN ANALYTICAL STUDY OF THE LOW-SPEED AERODYNAMICS OF STRAIGHT AND SWEPT WINGS WITH FLOW SEPARATIONAPPROVED FOR PUBLIC RELEASEDigital Resources/Online E-Resources |
| 20 |
Material Type: Reports
|
|
STEPLESS AND STEPPED PLANING HULLS-GRAPHS FOR PERFORMANCE PREDICTION AND DESIGNApproved for public release; distribution is unlimited.Digital Resources/Online E-Resources |
Results 1 - 20 of 143 for All Library Resources
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Creation Date
- Before 1950 (3)
- 1950 To 1952 (91)
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Resource Type
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Subject
- Aspect Ratio (136)
- Aerodynamics (51)
- Wings (51)
- Fluid Mechanics (35)
- Aircraft (32)
- Mach Number (31)
- Ati Collection (31)
- Sweptback Wings (27)
- Aerodynamic Characteristics (24)
- Lift (22)
- Drag (20)
- Angle Of Attack (19)
- Airfoils (17)
- Supersonic Characteristics (17)
- Pitch (16)
- Wind Tunnel Tests (16)
- Moments (15)
- Model Tests (14)
- Hydrofoils (14)
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Databases
- DTIC STINET (127)
- DTIC Technical Reports (127)
- Technical Report Archive and Image Library (TRAIL) @ UNT Digital Library (7)
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- Audio Visual Communication Review (1)
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