Longitudinal Static Stability And Drag Characteristics Of A 7d And F 4e Aircraft With Various External Store Configurations At Transonic Speeds
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External Store Airloads Prediction Technique
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Author : A. R. Rudnicki (Jr.)
language : en
Publisher:
Release Date : 1975
External Store Airloads Prediction Technique written by A. R. Rudnicki (Jr.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with Mach number categories.
Store Separation
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Author : Bertha M. Ryan
language : en
Publisher:
Release Date : 1973
Store Separation written by Bertha M. Ryan and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with Weapons systems categories.
Longitudinal Static Stability And Drag Characteristics Of A 7d And F 4e Aircraft With Various External Store Configurations At Transonic Speeds
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Author : Ronald E. Davis
language : en
Publisher:
Release Date : 1971
Longitudinal Static Stability And Drag Characteristics Of A 7d And F 4e Aircraft With Various External Store Configurations At Transonic Speeds written by Ronald E. Davis and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with categories.
Longitudinal aerodynamic characteristics of 0.05-scale models of A-7D and F-4E aircraft were obtained at Mach numbers from 0.50 to 1.30 to determine the effects of store configuration and location on stability and drag. Prototypes, as well as a family of proposed store configurations, were tested. (Author).
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1974
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Aeronautics categories.
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Government Reports Annual Index
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Author :
language : en
Publisher:
Release Date : 1978
Government Reports Annual Index written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1978 with Research categories.
Sections 1-2. Keyword Index.--Section 3. Personal author index.--Section 4. Corporate author index.-- Section 5. Contract/grant number index, NTIS order/report number index 1-E.--Section 6. NTIS order/report number index F-Z.
Longitudinal Static Stability And Drag Characteristics Of F 4d Aircraft With Various External Store Configurations At Transonic Speeds
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Author : D. K. Smith
language : en
Publisher:
Release Date : 1971
Longitudinal Static Stability And Drag Characteristics Of F 4d Aircraft With Various External Store Configurations At Transonic Speeds written by D. K. Smith and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with categories.
Force and moment data were botained with a 0.05-scale model of the F-4D aircraft at Mach numbers from 0.75 to l.30 to determine the effects of different store and rack configurations on the static stability and drag of the aircraft. Six proposed rack launchers and four proposed store shapes were tested for a total of 57 external loading configurations. (Author).
Longitudinal Stability Characteristics At Transonic Speeds Of A Canard Configuration Having A 45 Degree Sweptback Wing Of Aspect Ratio 6 0 And Naca 65a009 Airfoil Section
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Author : A. James Vitale
language : en
Publisher:
Release Date : 1954
Longitudinal Stability Characteristics At Transonic Speeds Of A Canard Configuration Having A 45 Degree Sweptback Wing Of Aspect Ratio 6 0 And Naca 65a009 Airfoil Section written by A. James Vitale and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Airplanes categories.
A flight investigation has been conducted to determine the longitudinal stability, lift, and drag characteristics at transonic speeds of a rocket-powered model of a canard configuration having a 45 degree swept-back wing of aspect ratio 6.0, taper ratio of 0.6, and NACA 65A009 airfoil section. The canard surface had an aspect ratio of 4.0 and 45 degrees of sweepback. The variations with Mach number of lift, drag, and longitudinal stability for the canard configuration are compared with a tailless and a conventional or tail-last model having the same wing.
Longitudinal Static Stability And Inlet Drag Characteristics Of The Mcdonnell Douglas F 15 Tactical Fighter Aircraft At Mach Numbers Of 1 60 And 2 20
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Author : F. J. Keeney
language : en
Publisher:
Release Date : 1971
Longitudinal Static Stability And Inlet Drag Characteristics Of The Mcdonnell Douglas F 15 Tactical Fighter Aircraft At Mach Numbers Of 1 60 And 2 20 written by F. J. Keeney and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with Eagle (Jet fighter plane) categories.
Longitudinal Stability Control Effectiveness And Drag Characteristics At Transonic Speeds Of A Rocket Propelled Model Of An Airplane Configuration Having An Unswept Tapered Wing Of Aspect Ratio 3 0 And Naca 65a004 5 Airfoil Sections
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Author : John C. Jr McFall
language : en
Publisher:
Release Date : 1953
Longitudinal Stability Control Effectiveness And Drag Characteristics At Transonic Speeds Of A Rocket Propelled Model Of An Airplane Configuration Having An Unswept Tapered Wing Of Aspect Ratio 3 0 And Naca 65a004 5 Airfoil Sections written by John C. Jr McFall and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with categories.
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
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Author : Kenneth W. Goodson
language : en
Publisher:
Release Date : 1961
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 has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Stability of airplanes, Longitudinal categories.
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.