|
Internal Flow Systems for Aircraft |
Rogallo F. M. |
|
Introduction To Aeroflexibility |
Rogallo F. M. |
Flex Wing |
Flex Wing: Promotional Article |
Capt. Graham R. L. |
NACA L-123 |
Charts For Determining Jet-Boundary Corrections For Complete Models In &- By !0-Foot Closed Rectangular Wing Tunnels |
Gillis C. L., Polhamus E. C., Grat Jr. J. L. |
TN D-443 |
Preliminary Investigation of a Paraglider |
Rogallo F. M., Lowry J. G., Croom D. R., Taylor R. T. |
TN-D-629 |
An Exploratory Study of a Parawing as a High-Lift Device for Aircraft |
Naeseth. Rodger L |
TN D-927 |
Free-Flight Investigation of Radio Controlled Models with Parawing's |
Hewes. Donald E. |
TN-D-983 |
Low Subsonic Pressure Distributions on Three Rigid Wings Simulating Paragliders with Varied Canopy Curvature and Leading-Edge Sweep |
Fournier. Paul G.. Bell. B. Ann |
TN-D-985 |
Wind-Tunnel Investigation of Paraglider Models at Supersonic Speeds |
Taylor. R. T. |
TN-D-1009 |
Transonic Pressure Distribution on three wings simulating Paragliders with varied canopy curvature and leading-edge sweep |
Bell. B. A.. Fournier. P. G. |
TN-D-1003 |
An analytical investigation of loads temperature and ranges obtained during the recovery of Rocket boosters by means of a parawing |
Hatch. H. G.. Jr.. Mc Gowan. W. A. |
TN-D-1022 |
A study of the Aerodynamic characteristics of a fixed geometry Paraglider configuration and three canopies with simulated variable canopy inflation at a Mach number of 6.6 |
Penland. J. A. |
TN-D-1255 |
Low-speed wind tunnel investigation to determine the flight characteristics of a model Parawing utility vehicle |
Johnson Jr., J. L., |
TR 62-3A |
Flexible Wing Cargo Gliders Vol I |
King. J. L. Fink. J. E. Craigo. C. E. |
TR 62-3B |
Flexible Wing Cargo Gliders Vol II |
Givens E. R. |
L-3242 |
Flexible Wing Research And Development |
Rogallo F. M. |
TN D-972 |
Experimental And Theoretical Studies Of The Effects Of Camber And Twist On The Aerodynamic Characteristics Of Parawing's Having Normal Aspect Ratios of 3 & 6 |
Polhamus E. C., Naeseth R. L. |
TR 62-65 |
Flexible-wing Manned Test Vehicle |
Briggs C. |
TN-D-1614 |
Experimental investigation of the Dynamic stability of a towed Parawing Glider model |
Shanks R. E. |
TN D-1826 |
Preliminary Flight Evaluation Of Two Unpowered Manned Paragliders |
Layton Jr., G. P., Thompson M. O |
TN-D-1618 |
Pressure distribution on three rigid wings simulating Parawing's with varied canopy curvature and leading edge sweep at Mach numbers from 2.29 to 4.65 |
Fournier P. G. |
TM-X-57480 |
Aerodynamics of the parawing |
Johnson J. L Jr. Sleeman, W. C. Jr. |
TN D-1932 |
Free flight investigation of the deployment, dynamic stability, and control of a 1/12 scale dynamic radio-controled model of a large booster and Parawing |
Burk Jr. M. B. |
TN D-1937 |
Low speed investigation of cable tension and aerodynamic characteristics of a Parawing and spacecraft combination |
Sleeman, W. C., Jr. |
TN D-1946 |
Full scale wind tunnel investigation of a Flexible-wing manned test vehicle |
Johnson Jr., J. L., Hassell Jr. J. L. |
TN D-1957 |
Low speed investigation of the effects of wing sweep on the aerodynamic characteristics of Parawing's having equal length kell |
Naeseth R. L., Gainer G. T. |
AD 431128 |
Operational Demonstration and Evaluation of the Flexible Wing Precision Drop Glider In Thailand, March-July 1963 |
Quinn W. R. |
TN D-2031 |
Low-subsonic flight characteristics of a model of a supersonic-airplane configuration with a Parawing as a landing aid |
Johnson Jr., J. L., |
TN D-2044 |
Free-flight investigation of a Parawing recovery device for a radio-controlled 1/5-scale dynamic model spacecraft |
Libbey C. E. |
TM-X-51958 |
Stress and shape analysis of a paraglider wing |
Fralich R. W. |
AD B2522433 |
Pilot's Handbook for the Flexible Wing Aerial Utility XV-8A (Ryan Model 164) |
Unknown |
TN D-2291 |
Stalling and tumbling of a radio-controlled Parawing airplane model |
Libbey C. E., Johnson Jr., J. L., |
TN D-2346 |
Low-speed longitudinal aerodynamic investigation of Parawing's as auxiliary lifting device for a supersonic airplane configuration |
Phillips W. P. |
TN D-2292 |
Experimantal investigation of the dynamic stability of a towed parawing glider air cargo delivery system |
Shanks, R. E. |
TN D-2551 |
Effects of canopy shape on low speed aerodynamic characteristics of a 55 degree swept Parawing with large-diameter leading edges |
Croom D. R., Naeseth R. L., Sleeman Jr., W. C. |
AD 477482 |
An Evaluation of Flex-Wing Aircraft in Support of Indigenous Forces Involved in Counterinsurgency Operations |
Wise R. A., et al |
TR 64-55 |
XV-8A Flexible Wing Aerial Utility Vehicle |
Kredit H. |
TR 64-74 |
XV-8A Flexible Wing Aerial Utility Vehicle |
Landgraf F. M. Girard P. F. |
TN D-2492 |
Low-speed force and flight investigation of a model of a modified Parawing utility vehicle |
Johnson Jr., J. L., |
TR 65-11 |
Flexible Wing Air Cargo Delivery System |
Sakamoto N. Cota G. |
TN D-2859 |
Low-speed wind tunnel test of a large scale inflatable structure Paraglider |
Gamse B., Mort K. R., Yaggy P. F. |
TN D-2922 |
Effects of aspect ratio and canopy shape on low-speed aerodynamic characteristics of a 50 degree swept parawing |
Bugg F. M. |
TM-X-56747 |
Resume of recent parawing research |
Croom. D. R.. Rogallo. F. M.. Sleeman Jr. W. C. |
CR-92224 |
Paraglider landing system test program final report |
CHRISTENSEN. N. R. SNODGRASS. RR |
TN D-2998 |
Low-speed force and flight investigation of various methods fro controlling Parawings |
Johnson Jr., J. L. |
TR 68-43-AD |
Preliminary Investigation of Concepts for Low-Altitude Airdrop of Personnel-Exploritory Development [Final Report] |
Lau R. A. |
TN D-3461 |
A theoretical analysis of the dynamic lateral stability and controln of a Parwing vehical |
Chambers J. R., Boisseau |
TN D-3493 |
Low-speed tests of 50 drgree-swept Parawings applied to a 1.17-scale model of a manned flight vehicle |
Bugg F. M. |
TN D-3442 |
Low-speed wind-tunnel and free-Flight drop test investigation of a Paraglider configuration having large tapered leading edges and keel |
Croom D. R., Fournier P. G. |
AD 803668 |
Final Technical Report Sailwing Wind Tunnel Test Program |
Sweeny T. E., Ormiston R. A., Mercer J. E., Jobst A. |
TM-X-59738 |
NASA research on flexible wings |
Rogallo. F. M. |
TN D-3673 |
Wind-Tunnel investigation of the flight characteristics of a model of an aspict-ratio-6 conical Parawing utility vehicle |
Smith Jr., C. C., Ware G. M. |
TN L-5419 |
NASA Research on Flexible Wings |
Rogallo F. M. |
TN D-3960 |
Wind-Tunnel tests of a series of parachutes designed for controilable glider flight |
Wieberg J. A., Mort K. W. |
TN D-3856 |
Wind-Tunnel investigation of the static aerodynamic characteristics of an 18-foot (5.49meter) all flexible Parawing |
Libbey C. E., Haeseth C. E., Ware R. L. |
| TN D-3869 |
Gemini Landing Systems Development program March 1967 |
Leyland C. Norman |
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Low-speed wind tunnel investigation of tension-structure Parawing |
Naeseth R. L., Fournier P. G. |
TN D-4010 |
Low-speed tests of an all-flexible Parawing for landing a lifting-body spacecraft |
Bugg F. M., Sleeman Jr. W. C. |
TN D-4062 |
Full-scale investigation of the aerodynamic characteristics of a model employing a Sailwing concept |
Fink M. P. |
TN D-4182 |
Static aerodynamic characteristics of three Ram-Air-Inflated low-aspec-ratio fabric wing |
Sanger Jr., M. B., Ware R. L. |
TN D-4530 |
Investigation of copacitance-typemmeteoroid detector using an inflatable Paraglider |
Siviter Jr., J. H. |
TN D-4672 |
Wind-tunnel investigation of the static aerodynamic characteristics of a multilobe gliding parachute |
Libbey C. E., Ware R. L. |
TN D-4665 |
Experimental verification of scale factors for Parawing opening chatacteristics |
Eichblatt D. L., Moore R. H., Barton R. L. |
CR-1166 |
Investigation of methods for predicting the aerodynamic characteristics of two-lobed parawings |
Mendenhall. M. R. Nielsen. J. N. Spangler. S. B. |
TN D-4724 |
Free-flight and wind-tunnel studies of deployment of a dynamically and elastically scaled inflatable parawing model |
Ferris A. T., Kelly H. N. |
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Parasev Instruments and Electronic Systems Implementation for Gemini Parasail Retrorocket |
Manned Space Craft Centre |
TN D-5031 |
Investigation of opening characteristics of an all-flexible parawing |
Gainer T. G. |
TN D-5049 |
Fixed-base visual simulation of pilot controlled descents of an advanced Apollo spacecraft with an all-flexible parawing |
Jaquet B. M., Miller Jr. G. K., Price D. B. |
Mar 1969 |
NASA Technical Note |
Langley RC |
TN D-5071 |
Experimental verification of scale factors for parawing opening characteristics with dimensional ratios from 1/1.3 to 1/3 |
Eichblatt D. L., Hughes T. F., Moore R. H. |
Mar 1969 |
NASA Technical Note |
MSC Houston |
TN D-5199 |
Wind-tunnel investigation of the aerodynamic characteristics of a twin-keel parawing |
Wate G. M. |
May 1969 |
NASA Technical Note |
Langley RC |
CR-66879 |
Wind tunnel and free flight investigation of all-flexible parawings at small scale |
Buhler W. C.. Linhart E. M. |
June 1969 |
NASA Contractor Report |
Northrop Corp, Ventura Division |
CR-66918 |
Free flight investigation of large all- flexible parawings and performance comparison with small parawings Final report |
Gran. W. M.. Linhart. E. M.. Moeller. J. H.. Parson. L. T. |
Mar 1970 |
NASA Contractor Report |
Northrop Corp, Ventura Division |
TN D-5708 |
Wind-tunnel investigation of several large- scale all-flexible parawings |
Falarski M. D., Mort K. W. |
Mar 1970 |
NASA Technical Note |
Army ARL & Ames RC |
TN D-5793 |
Performance and deployment characteristics of a twin-keel parawing with various amounts and permeabilities of porous material in outer lobes |
Morgan Jr., H. L. |
May 1970 |
NASA Technical Note |
Langley RC |
TN D-5900 |
Determination of inflated shape and inertial properties of an all-flexible parawing |
Gloss B. B. |
June 1970 |
NASA Technical Note |
Langley RC |
TN D-5911 |
Aerodynamic and deployment characteristics of single-keel solid and single-keel slotted personnel parawings |
Bradshaw C. F., Morgan Jr. H. L. |
July 1970 |
NASA Technical Note |
Langley RC |
TN D-5940 |
Fixed-base visual simulation of obstacle avoidance during terminal descent of advanced Apollo spacecraft with an all-flexible parawing |
Miller Jr. G. K. |
Aug 1970 |
NASA Technical Note |
Langley RC |
TN D-5893 |
Model wind-tunnel and flight investigation of a parawing lifting body landing system |
Naeseth R. L. |
Oct 1970 |
NASA Technical Note |
Langley RC |
TN D-5936 |
Low-speed wind-tunnel investigation of a series of twin-keel all-flexible parawings |
Naeseth R. L. |
Oct 1970 |
NASA Technical Note |
Langley RC |
TN D-5965 |
Low-speed wind-tunnel investigation of all- flexible twin-keel tension-structure parawings |
Fournier P. G. |
Oct1970 |
NASA Technical Note |
Langley RC |
TN D-5974 |
Wind tunnel studies of effects of construction methods design details and canopy slots on the aerodynamic characteristics of small-scale all-flexible parawings |
Fournier P. G. Sleeman W. C. Jr. |
Oct 1970 |
NASA Technical Note |
Langley RC |
CR-1674 |
An exploratory aerodynamic and structural investigation of all-flexible parawings |
Lee A. L. Nielson J. N. Spangler S. B. Stahara S. S. |
Dec 1970 |
NASA Contractor Report |
Nielson Engineering & Research |
TN D-6306 |
Aerodynamic and deployment characteristics of multistage canopy and suspension-line reefing systems for a twin-keel all-flexible parawing |
Mc Hatton A. D. Morgan H. L. Jr |
June 1971 |
NASA Technical Note |
Langley RC |
CR-1767 |
Section data for thin highly cambered airfoils in incompressible flow |
Milgram J. H. |
July 1971 |
NASA Contractor Report |
Mass. Inst. of Tech. for LRC |
CR-1788 |
Geometric aerodynamic and kinematic characteristics of two twin keel parawings during deployment |
Churchill F. T. Holt R. B. Kenner P. M. |
Aug 1971 |
NASA Contractor Report |
Vought M & S Div. LTV Aerospace Corp. |
TM X-2307 |
Deployment loads data from a free flight investigation of all-flexible parawings at small scale |
Croom D. R. |
Aug 1971 |
NASA Technical Memorandum |
Langley RC |
TM X-2326 |
Deployment loads data from a free flight investigation of all-flexible parawings having 371.612 Meters sq. (4000 feet sq.) of wing area |
Croom D. R. |
Nov 1971 |
NASA Technical Memorandum |
Langley RC |
AD B 126450 |
From Delta Glider to Airplane |
unknown Russian |
Jan 1988 |
Translated Russian Article |
US Army Intelligence |
TM X-4525 |
The Development and Flight Test of a Deployable Precision Landing System for Spacecraft Recovery |
Sim A. G., Murray J. E., Neufeld D. C., Reed R. D. |
Sept 1993 |
NASA Technical Memorandum |
Dryden Flight RF |
RD-ST-95-9 |
Materials Analysis of Foreign Produced Flex Wings |
Ingram A. S. |
Mar 1995 |
Technical Report |
Structures Directorate Research |
. |
Flexible Wings For Transportation 1972 |
Rogallo F. M. |
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