Invented in Grafton 1963

THE

AUSTRALIAN

HANG GLIDING HISTORY

Experienced by the World

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N.A.S.A. Technical Reports and Presentations  

Tr-713

Internal Flow Systems for Aircraft

Rogallo F. M.

I.T.A.

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

TN D-3940

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 mod

Ferris A. T., Kelly H. N.

N 75-70841

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.

Continued

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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